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 HALA0700250Skin · crackedON NR 1 ENGINE CHANGE, LT PYLON APRON UPPER AFT LATCH CUTOUT IS CRACKED. REPAIRED CRACK PER HAL M105 B10192.SDR AMWA7026CSkin · chafedFRICTION CHAFING DURING OPERATION HAS CAUSED WORN SEGMENTS ON THE RT NACELLE (TURTLEBACK) SKINS. REPAIRED IAW REPORT 6702-5 REV 1R.SDR AMWA7026BSkin · chafedFRICTION CHAFING DURING OPERATION HAS CAUSED WORN SEGMENTS ON THE LT NACELLE (TURTLEBACK) SKINS. REPAIRED IAW REPORT 6702-5 REV 1R.SDR UIEA200700245Skin · crackedNR 3 PYLON OVAL PANEL 473AR CUTOUT CRACKED LOWER AFT SKIN. NR 3 PYLON OVAL PANEL 473AR CRACKED SKIN REPAIRED AS PER BOEING MESSAGE 1-351859671-9 AND FAA FORM 8100-9.SDR DHL2007803539Skin · wornNR 2 ENG NACELLE INLET COWL UPPER SIDE WORN, STA YN 147.534 AT 12 O'CLOCK POS. PERFORMED MAJOR REPAIR IAW SRM 71-5-2 FIG 2. REMOVED FASTENERS IAW SRM 51-1-21A. CUT OUT DAMAGED SECTION AND FABRICATED NEW SKIN SEGMENT (AL2024T3 0.080") AND STEEL SPLICE 17.7 PSDR DHL2007803541Skin · wornNR 1 ENG NACELLE INLET COWL UPPER SIDE WORN, STA YN 147.534 AT 12 O'CLOCK POS. PERFORMED MAJOR REPAIR IAW SRM 71-5-2 FIG 2. REMOVED FASTENERS IAW SRM 51-1-21A. CUT OUT DAMAGED AREA AND FABRICATED NEW SKIN SEGMENT (AL2024T3 0.080") AND STEEL SPLICE 17-7PH 0.SDR DHL2007803540Skin · wornNR 4 ENG NOSE COWL EXT SKIN WORN (STA YN 147.000 - 157.000 AT 12 O'CLOCK POS LT/RT) MAJOR REPAIR. PERFORMED MAJOR REPAIR IAW SRM 71-5-2 FIG 2. REMOVED FASTENERS IAW SRM 51-1-21A. CUT OUT DAMAGED SECTION AND FABRICATED NEW SKIN SEGMENT (AL2024T3 0.080") AND SDR DHL2007803538Skin · wornNR 3 ENG NOSE COWL EXTERNAL SKIN WORN (STA YN 147.534, AT 12 O'CLOCK POS) MAJOR REPAIR. PERFORMED MAJOR REPAIR IAW SRM 71-5-2 FIG 2. REMOVED FASTENERS IAW SRM 51-1-21A. CUT OUT DAMAGED SECTION AND FABRICATED NEW SKIN SEGMENT (AL2024T3 0.080") AND STEEL SPLISDR 07FDEA02088Panel · crackedCRACK (L<25MM) ON PYLON NR 2, RIB 8, OUTBOARD SIDE DOUBLER REPAIR PERFORMED IAW SB 54-6015 AND DWG R546-10124, APPROVED BY EA 6-5451-103251.SDR UPS07450016Skin · damagedINSPECTION TYPE:C NR 1 PYLON STRUT O/B LOWER EDGE SKIN FOUND DAMAGED AT STA 236. NR 1 PYLON STRUT O/B LOWER EDGE SKIN REPAIRED AT STA 236 AS PER SRM 54-34-03 FIG 25.SDR AMTA200700269Skin · damagedNR 2 PYLON LOWER SIDE STRUCTURE EXPOSED TO HIGHT HEAT IN AREA OF HP-6 ENGINE PNEUMATIC DUCT AREA. AREA WAS REPAIRED IAW ERA 757-54R-6102 AND SAA EA 757-54-00-09-AO778, DATED 4-20-07, FAA FORM 8100-9/ 337 TIME LIMITED. REPAIR FROM 4/20/07 VALID FOR 24 MONTHS.SDR KCSA071172Angle · crackedNR 1 PYLON NAC STA-221 O/B ANGLE CRACKED FWD SIDE OF BULKHEAD.SDR 2007UALA01709Panel · delaminatedLEFT INBOARD PYLON PANEL IS DELAMINATED & MISSING RIVETS. [07-10-07] REMOVED LEFT INBD PYLON PANEL & CREATED DOUBLER REPAIR PER SRM. INSTALLED DOUBLER, REINSTALLED PANEL. INSTALLED LEADING EDGE FASTENERS TO COMPLETE INSTALLATION OF PANEL. SUSPECT VIBRATIOSDR FDKA200705245Skin · chafedRIGHT ENGINE, LOWER COWLING, IS CHAFED, OUT OF LIMITS, AT THE AFT END ON THE INNER SKIN. THE DAMAGE HAS BEEN REPAIRED.SDR NWAA072245646Skin Panel · crackedDURING "M" CHECK FOUND CRACK IN NR 2 PYLON RT SKIN PANEL ASSEMBLY HOLE CUTOUT NEAR NAC STA 132. REPAIRED PER EA 56-194174.SDR EIA2007106Skin · crackedUPPER EDGE OF NR 2 PYLON ACCESS PANEL 463AR OPENING IS CRACKED AND WORN. REMOVED DAMAGE, NDT AREA, FABRICATED AND INSTALLED REPAIR PER ECRA 487-54-043-2.SDR EIA2007103Skin · crackedNR 4 PYLON O/B ACCESS PANEL CUTOUT FLANGE CRACKED, PYLON STATION 213.6. REMOVED DAMAGE, NDTD AREA, FABRICATED AND INSTALLED REPAIR PER ECRA 487-54-046-2.SDR USAA070376Skin · crackedFWD UPPER CORNER OF ACCESS PANEL 5724L OPENING, PYLON SKIN HAS CRACK. INSTALLED REPAIR DOUBLER PER TR 54-50-07, DEFECT SIZE: .125 INCH.SDR UPS07549874Skin · crackedINSPECTION TYPE:C NR 1 PYLON LEFT SIDE FWD SKIN HAS STOP DRILLED CRACK & REPAIR DOUBLER. OPEN STOPDRILL HOLE BY 1/32 PER PRELIMINARY 1 EA 757-5451-27-A1674 STEP 2. NOTE: NO PLUG REQUIRED FOR NEW DOUBLER, NO HOLE EXISTS. ACCOMPLISHED PER FINAL EA 757-5451-2SDR AMWA06033DSkin · chafedFRICTION CHAFFING OCCURED DURING ENGINE OPERATION RESULTING IN WORN SEGMENTS ON THE LT ENGINE UPPER AFT NACELLE ALONG ENTIRE LENGHT & SHAPE OF NACELLE. REPAIRED IAW ENGINEERING AUTHORIZATION REPAIR DWG 1900D142-1 REV 1R.SDR AMWA06033CSkin · chafedFRICTION CHAFFING OCCURED DURING ENGINE OPERATION RESULTING IN WORN SEGMENTS ON THE RT ENGINE UPPER AFT NACELLE ALONG ENTIRE LENGTH & SHAPE OF NACELLE. REPAIRED IAW ENGINEERING AUTHORIZATION REPAIR DWG 1900D142-1 REV 1R.SDR FDKA200705233Skin · chafedRIGHT LOWER COWL INTERNAL SKIN IS DAMAGED BEYOND LIMITS BETWEEN FRAMES 6&7 AT CENTER LINE. REPAIRED SKIN.SDR FDKA200705232Skin · chafedRIGHT LOWER COWL INTERNAL SKIN IS DAMAGED BEYOND LIMITS BETWEEN FRAMES 4&5 AT CENTER LINE. REPAIRED SKIN.SDR FDKA200705228Cowling · chafedLT LOWER COWLING IS CHAFED, OUT OF LIMITS AT FRAME NR 6. THE DAMAGE HAS BEEN REPAIRED.SDR QXEA200700757Skin · damagedC4 PDX - JOBOLTS HAVE WORKED THRU TOP SKIN PANEL AND BUTT STRAP, STATION XN210, LEFT NACELLE. REPAIRED IAW RD8/4-54-154, AND SRM 51-40-07, 51-42-05.SDR DL76L070389Fitting · crackedTHE NR 2 PYLON CLOSE OUT ANGLE WAS FOUND CRACKED AND THE MIDSPAR FITTING WAS DAMAGED DURING ANGLE REMOVAL. THE CRACKED ANGLE WAS REPLACED AND THE MIDSPAR FITTING WAS REPLACED PER S/B 767-54-0080.SDR 2007UALA01359Skin · crackedNR 2 PYLON INBOARD SKIN IS CRACKED AT THE MOST FWD ACCESS HOLE, 2:00 O'CLOCK POSITION. [SUP 06-06-07] ACCOMPLISHED REPAIR WITH UA ENGINEERING SPECIFICATION.SDR DL76L070384Angle · crackedTHE NR 2 PYLON CLOSEOUT ANGLE WAS FOUND WITH A CRACK IN THE OUTBOARD SIDE. THE MIDSPAR FITTINGS ALSO HAD TOOLING DAMAGE. THE DAMAGED ANGLE WAS REPAIRED WITH REPAIR STRAPS.SDR 2007UALA01318Skin · crackedNR 2 ENG PYLON PNL CUT OUT CRACKED AT UPR FWD CORNER LOCATED ON I-B PYLON SKIN ACCESS HOLE CUT OUT JUST FWD OF HYD BAY. MAJOR REPAIR ACCOMPLISHED: STOP DRILLED CRACK. FABRICATED & INSTALLED DOUBLER REPAIRS.SDR CALA0700190Plate · crackedNR 1 ENGINE PYLON PANEL OPENING FOR PANEL 5724 CRACKED. REPAIRED IAW ECRA 5431-01034.SDR USAA070294Access Panel · crackedLEFT PYLON ACCESS PANEL 5727L ON OUTER SKIN HAS CRACK. INSTALLED DOUBLER PER TR 54-30-07, DEFECT SIZE: 1 INCH.SDR NWAA071595501Skin Panel · crackedDURING "M" CHECK, FOUND CRACK IN 2 PYLON RT SKIN PANEL LIGHTING HOLE AT NAC STA 133. REPAIRED PER EA 55-208817.SDR AMWA28025Skin Panel · wornRT NACELLE SKIN CAUSED FRICTION WEAR DAMAGE. REPAIRED IAW DESIGNATED ER DRAWING 1900D 162-1 REV 1R AND BSRM 51-40-02 AND 51-40-03.SDR WRLA2007059Skin · crackedDURING 4C+12A CHECK, EGAT MECHANIC FOUND CRACK ON NR 2 ENGINE INLET COWL INNER SKIN AT 6 O'CLOCK POSITION 1EA, 7 O'CLOCK POSITION 4EA, 8 O'CLOCK POSITION 3EA, 10 O'CLOCK POSITION 1EA, 11 O'CLOCK POSITION 2EA AND 12 O'CLOCK POSITION 1EA. [SUP 05-02-07] REPAIRSDR 07FDEA01443Panel · cracked(N0535) CRACK FOUND ON NR 1 PYLON AFT FAIRING. REPAIR ON GOING AS SRM. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS MINOR. FAIRING TO PYLON COWL OF RT CORE W/ TWO CRACKS REPAIRED IAW SRM 54-56-10 CONFIG 2 FIG 201.SDR 07FDEA01403Panel · crackedCRACKS ON PYLON NR 2 LATERAL PANEL AT RIB 8 RT. REPAIR WAS PERFORMED IAW SRM 54-51-31/FIG 201, APPROVED BY EA 6-5450-101300.SDR 07FDEA01402Panel · crackedCRACK FOUND ON PYLON NR 1 LATERAL PANEL AT RIB 8 LT/RT. REPAIR WAS PERFORMED IAW SRM 54-51-31/FIG 201, APPROVED BY EA 6-5450-101299.SDR 07FDEA01404Panel · corrodedCORROSION ON PYLON NR 2 INBOARD SIDE PANEL, RIB 10-18. REPAIR PERFORMED BY BLEND OUT IAW EA 6-5451-101322 AND RAS 045345/010/2006 ISSUE "A".SDR NWAA071696744Skin · crackedDURING "M" CHECK, FOUND CRACKS IN NR 4 PYLON SKIN AND STIFFENER AT NAC STA 218 AND ACCESS PANEL 483CL CUTOUT. REPAIRED PER EA 67-209238.SDR VOX2007F00000Cowling · damagedUPPER RT COWLING CAME OPEN IN FLIGHT. RECOMMEND INSTALLING 2 SCREWS AT LEADING EDGE OF COWLING TO PREVENT THIS HAPPENING. (K)SDR USAA070253Skin · crackedCRACK IN INBOARD PYLON, LOWER AFT CORNER, CUTOUT FOR ACCESS PANEL 5724L. INSTALLED DOUBLER PER TR 54-50-07, DEFECT SIZE: .375 INCH.SDR 07FDEA01190Skin · dentedFOUND REPAIR AT THE TE OF THE NR 1 ENG PYLON STUB FRAME UPPER SURFACE EXISTING. REPAIR DID NOT CONFORM TO SRM 54-30-2. REMOVED EXISTING REPAIR ON UPPER SURFACE. REMOVED DAMAGE SKIN, REMOVED DAMAGE ON LOWER SURFACE T/E SKIN. REPAIRED UPPER AND LOWER T/E WEDSDR USAA200703005Skin · crackedA .75 INCH CRACK FOUND AT LEFT PYLON AT ACCESS PANEL 5727L OPENING. STOP DRILLED & INSTALLED DOUBLER PER TYPICAL REPAIR 54-30-07.SDR KCSA071078Structure · wornNR 3 PYLON O/B SIDE STA 180 LOWER SKIRT CORNER WORN AWAY.SDR KCSA071076Skin · wornNR 4 PYLON O/B SKIN WORN AT LOWER SKIRT AT NAC STA 236.SDR KCSA071075Skin · wornNR 3 PYLON I/B SKIN AND FIRESHIELD WORN ON LOWER SKIRT AT NAC STA 233.SDR CA070322001Panel · cracked(CAN) PANEL IS INSTALLED ON RT IB SIDE OF NACELLE. IT COVERS THE FUEL FIREWALL SHUTOFF VALVE. THE PANEL IS MANUFACTURED WITH A BULGE TO ACCOMMODATE THE VALVE. IN THIS INSTALLATION THE VALVE CONNECTOR PLUG CHAFFED AGAINST THE PANEL CAUSING A STRESS RISER RESULSDR NWAA071105508Skin · crackedDURING SCHEDULED ENGINE REPLACEMENT INSPECTION REVEALED CRACK IN THE NR 2 PYLON RT SKIN. REPAIRED PER EA 55-209137.SDR 07FDEA00809Skin · gougedPYLON NR 3: ABOVE ENGINE DRAIN PAN APPROX STA YN=230LH LOWER PYLON SKIN FOUND WITH SEVERAL GOUGES. COMPLIED WITH FEDEX EA 1-5450-109842, CLASSIFIED AS MAJOR REPAIR AS PER FEDEX GMM 6-2-100.SDR 07FDEA00808Skin · gougedPYLON NR 3: ABOVE ENGINE DRAIN PAN APPROX STA YN230 RT LOWER PYLON SKIN FOUND WITH SEVERAL GOUGES. COMPLIED WITH FEDEX EA 1-5450-109841, CLASSIFIED AS MAJOR REPAIR AS PER FEDEX GMM 6-2-100.
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