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.

SDR DLM88002267Spar · corrodedTHE NR 2 PYLON FRONT SPAR UPPER AND LOWER LUGS WERE OVERSIZED TO REMOVE CORROSION. THE UPPER LUG WAS OVERSIZED TO 1.3695 AND THE LOWER LUG WAS OVERSIZED TO 1.3705. ERA 396435-14 OVERSIZES THE BORE AND INSTALLS A REPAIR BUSHING. THE DAMAGE WAS FOUND AT HMV.Nov 20, 2000 · N937DL · Doug MD88SDR CALA0001751Angle · crackedINSPECTION FOUND A 1 INCH CRACK IN RIGHT PYLON PANEL 8212C L-ANGLE. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-10-4 AND 51-30-2.Nov 13, 2000 · N14840 · Doug DC982SDR CALA0001694Angle · crackedINSPECTION FOUND A 1 INCH CRACK AT EACH END OF LT PYLON PANEL NR 8111C ATTACH SUPPORT ANGLE. THE SUPPORT ANGLE WAS REMOVED AND A NEW SUPPORT ANGLE WAS INSTALLED IAW SRM 51-10-3 AND 51-30-2.Nov 6, 2000 · N14840 · Doug DC982SDR C2XAOOCL088O-Ring · deterioratedCREW REPORTED NR 1 ENGINE BLEED LEAK MESSAGE WHILE IN CRUISE. THEY ALSO REPORTED A LOSS OF PRESSURIZATION WITH THE ENGINE BLEEDS. THIS OCCURRED WHILE SELECTING NR 1 ENGINE BLEED VALVE OPEN. THE CREW DECLARED A EMERGENCY AND DIVERTED INTO ERI. A/C LANDED WITHOUOct 29, 2000 · N14505 · Emb EMB135ERSDR CALA0001635Air Box · crackedINSPECTION FOUND A 2 INCH CRACK IN LOWER CENTER PYLON AIR BOX WHERE THE PRECOOLER AIR DUCT ATTACHES (I/B SIDE). THE CRACKED AREA WAS CUT OUT AND A REPAIR WAS INSTALLED IAW SRM 54-20-00, FIGURE 19A.Oct 23, 2000 · N12064 · Doug DC1030SDR AALA20001743Structure · cutTUL - FOUND UPPER PYLON CHORD ANGLE CUT FROM 11 INCHES AFT STATION 1183. SPLICED IN CHORD ANGLE REPAIR PER SRM 51-40-3. (M)Oct 19, 2000 · N883AA · Boeing 727223SDR RRXA003176Structure · wornDURING A MAINTENANCE VISIT FOUND A WORN EDGE ON THE AFT NR 2 ENGINE LT PYLON SKIRT, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.Oct 6, 2000 · N957R · Doug DC863FSDR MALA000624Duct · crackedFOUND DURING C-CHECK, RT ENGINE INBOARD NACA DUCT CRACKED AT PANEL 463AL. REFER TO CELSIUS TASK CARD 4535, W/O 18843 AND SAAB STATEMENT 340 SDS000144. MAINTENANCE REPAIRED DAMAGE REF SAAB STATEMENT 340SDS000144. PERFORM NDT PER FFVNDT006EC NO CRACKS PAST ROSep 26, 2000 · N416XJ · Saab 340BSDR TWAA0015002Strap · damagedTHE RT PYLON RT AFT UPPER CAP STRAP AND RELATED STRUCTURE HAD OVERSIZED HOLES IN EXCESS OF THE NUMBER AUTHORIZED. REPAIRED PER EMLR 71221. UPPER CAP STRAP AND STRUCTURE REWORKED. CHECK-C 8-2-00 MCI.Sep 26, 2000 · N921L · Doug DC932SDR QXEA0002543Angle · chafedYXX- LEFT HAND HORSE COLLAR HAS CHAFE DAMAGE AT LOWER FORWARD ANGLE AT STATION XN60.00 AND YW 164.00. REPAIRED IAW DHC-8 SRM 51-20-11, AND EA 9-54-257, AND RD8-54-1346.Sep 14, 2000 · N824PH · Dhav DHC8102SDR UPS00434112Stiffener · crackedINSPECTION TYPE:C, NR 1 STRUT STIFFENER CRACKED AT VERT BULKHEAD NAC STA 180. NEW BRACKET FABRICATED IAW SRM 51-40-02 AND INSTALLED IAW SRM 51-30-02.Sep 8, 2000 · N691UP · Boeing 747121SDR L1GA200000296Support Bracket · crackedA 3 INCH CRACK NR 2 PYLON HYD LINE AREA.Aug 25, 2000 · N12507 · Doug DC932SDR L1GA200000295Angle · crackedA 1 INCH CRACK NR 2 PYLON ELEC COMP FWD I/B CORNER. FABBED REPAIR DOUBLERS.Aug 25, 2000 · N12507 · Doug DC932SDR L1GA200000294Web · crackedA 1 INCH CRACK NR 1 PYLON ELEC COMP AFT O/B CORNER. FABED REPAIR ANGLE.Aug 25, 2000 · N12507 · Doug DC932SDR QXEA0002366Structure · looseYXX- RIGHT HAND NACELLE TO REAR SPAR INBOARD AND OUTBOARD END OF LINK HAS LOOSE HARDWARE. REPLACED WORN HARDWARE AS PER DHC-8 100 MM.Aug 18, 2000 · N822PH · Dhav DHC8102SDR QXEA0002358Structure · looseYXX- LEFT HAND NACELLE TO REAR SPAR INBOARD AND OUTBOARD END OF LINK HAS LOOSE HARDWARE. REPLACED WORN HARDWARE PER DHC-8 MM.Aug 18, 2000 · N822PH · Dhav DHC8102SDR GAIA00504Start Valve · malfunctionedDISCREPANCY: IN CLIMB, THE NR 3 ENGINE START VALVE LIGHT ACME ON. PERFORMED ENGINE SHUT DOWN AND DECLARED AN EMERGENCY. AIRCRAFT RETURNED TO MHR AND LANDED WITHOUT FURTHER DIFFICULTIES. RAN NR 3 ENGINE THREE TIMES AND VERIFIED START VALVE OPEN AND CLOSING.Aug 17, 2000 · N180AX · Boeing 727222SDR AALA20001402Strap · crackedTUL - FOUND CRACK TWO PLACES, 2 LAYER AT 7 O CLOCK APPROX .125, 3 LAYER AT 4 O CLOCK. REPAIRED PER ESO 11697 DATED 8-11-00. INSTALLED 2 STRAPS ONE .071, THE OTHER .063. (M)Aug 14, 2000 · N706AA · Boeing 727223SDR MALA000528Scoop · crackedFOUND DURING C-CHECK, RT NACELLE FWD OUTBOARD COWL DOOR NACA SCOOP CRACKED IN THE AFT CORNER.Aug 13, 2000 · N446XJ · Saab 340BSDR QXEA0002355Structure · crackedYXX- RIGHT HAND NACELLE FOUND TO HAVE TWO CRACKS ABOVE ACCESS HOLES FOR MAIN LANDING GEAR RETRACT ACTUATOR ATTACH HARDWARE. REPAIRED IAW DHC-8 RD 8-54-109 PAGE 3 AND 4, SRM 54-00-00 PAGE 1 AND 20-21-18.Aug 12, 2000 · N822PH · Dhav DHC8102SDR QXEA0002353Structure · crackedYXX- CRACKED STRUCTURE ON NR 2 NACELLE BETWEEN MID DOOR''S FORWARD HINGE AND FORWARD BRACKET OF EXTENSION HANDLE. REPAIRED IAW DHC-8 RD 8-54-239 AND SRM 51-40-11 PAGES 1-4 AND 32-10-21.Aug 12, 2000 · N822PH · Dhav DHC8102SDR AALA20001385Web · crackedTUL - FOUND STATION 1380 AFT ENGINE PYLON SUPPORT (WEB) LEFT SIDE CRACKED AFT OF COCKPIT TEMP CONTROL VALVE. AARD 53-10-00-28. INSTALLED DOUBLER. (M)Aug 8, 2000 · N562AA · Doug DC983SDR L1GA200000183Attach Angle · crackedRIGHT HAND PYLON AFT BULKHEAD ATTACH ANGLE O/B END CRACKED. FABRICATED NEW REPAIR, TREATED AND PRIMED AND INSTALLED REPAIR.Aug 1, 2000 · N33506 · Doug DC932SDR UPS00833476Angle · crackedINSPECTION TYPE:N/A, 3 INCH CRACK IN NR 2 PYLON SKATE ANGLE. *S/D* REMOVED CRACKED SKATE ANGLE. LOCATED AND DRILLED AND INSTALLED NEW SKATE ANGLE IAW DWG AND DC8 SRM 51-1-24.Jul 29, 2000 · N808UP · Doug DC873FSDR UPS00434075Intercostal · crackedINSPECTION TYPE:C, NR 4 ENG PYLON NAC STN 150 APPROX INTERCOSTAL ACROSS FWD FIRESEAL CRACKED. NEW INTERCOSTAL FABRICATED IAW EO100830 AND FITTED IAW SRM 51-30-02.Jul 20, 2000 · N691UP · Boeing 747121SDR UPS00433998Angle · damagedINSPECTION TYPE:C, CARRY OUT PERMANENT REPAIR TO NR 2 PYLON AS PER EO B747-5430-12183. REPAIR CARRIED OUT IAW QUERY NOTE 15/2000. TRIM OUT RIB FLANGE AND SKIN ASSY, INST FREEZE PLUGS AND FABRICATE NEW REPAIR ANGLE AND FILLERS FROM 7075T6.Jul 12, 2000 · N691UP · Boeing 747121SDR DL767001319Skin · crackedCRACK INDICATIONS FOUND IN THE NR 1 AND NR 2 PYLON O/B SIDELOAD FITTING HOLES. BY REMOVING THE RT WING SKIN PANEL LAYER, IT WAS FOUND THAT THE CRACK INDICATION WAS CAUSED BY AN ENLARGED HOLE IN THAT LAYER, WHICH ACTS AS A SHIM IN THE STACKUP. NO CRACK INDICAJul 5, 2000 · N114DL · Boeing 767232SDR DL73K001264Panel · missingUPON ARRIVAL FOUND 01 O/B PYLON PANEL 5126L MISSING. REPLACED SAME.Jul 5, 2000 · N242WA · Boeing 737247SDR USAA000960Channel · crackedPIT - FOUND U-CHANNEL CRACKED 1 INCH, U-CHANNEL SUPPORT PYLON MID SECTION RIGHT WING NAC 145.63. LOCALLY MFG U-CHANNEL PER EA 55424 AND SRM 51-40-02. (M)Jun 26, 2000 · N375US · Boeing 7373B7SDR USAA000963Support Bracket · crackedPIT - FOUND SUPPORT ANGLE CRACKED 1 INCH AND CHAFED 6 INCHES BY 2 INCHES, RIGHT ENG PYLON SUPPORT STRUCTURE FOR PANEL 5842. INSTALLED SPLICE PLATE PER SRM 54-50-71 AND SRM 51-40-02. (M)Jun 26, 2000 · N375US · Boeing 7373B7SDR USAA000965Support Bracket · corrodedPIT - FOUND SUPPORT ASSEMBLY CORRODED 10 INCHES, ATTACH FLANGE ANGLE FOR PYLON PANEL 57422. REMOVED AND REPLACED CHAFE STRIP PER SRM 51-40-00. CORROSION LEVEL 2. (M)Jun 26, 2000 · N375US · Boeing 7373B7SDR UPS00233113Angle · crackedINSPECTION TYPE:C+SI ENGINE NR 2 AFT MOUNT SUPPORT RIB RIGHT CHORD INSIDE THE VERTICAL FIN HAS CRACKED SUPPORT ANGLE APPROX 17 INCHS FROM TOP OF CHORD. REPLACED CRACKED ANGLE IAW DRAWING NO.65-17553Jun 8, 2000 · N954UP · Boeing 727185CSDR AALA20001012Angle · gougedTUL - FOUND LEFT AFT ENGINE PYLON SUPPORT STATION 1380, FORWARD SIDE SUPPORT LOWER CHORD ANGLE IS DEEPLY GOUGED BEYOND LIMITS DUE TO IMPROPER POSITIONING OF COCKPIT TEMP CONTROL VALVE. LOCATED BELOW L-4 - L-5 LEFT. INSTALLED DOUBLERS WET AT STATION 1380, FORJun 7, 2000 · N286AA · Doug DC982SDR MALA000394Rib · chafedFOUND DURING C-CHECK THE RT NACELLE COWL PANEL 463DR HAS A CHAFED RIB JUST AFT OF BLEED PRE-COOLER INTAKE. MAINTENANCE BLENDED CHAFED AREA IAW SRM 51-10-10. TREATED AND PRIMED IAW SRM 51-20-42 & 51-20-40. FABRICATED REINFORCEMENT ANGLE IAW THE PRINCIPAL OF Jun 5, 2000 · N443XJ · Saab 340BSDR AALA20001005Shear Tie · crackedTUL - FOUND ENGINE PYLON SHEAR TIE CRACKED BELOW LONGERON 14R SHEAR TIE ALSO HAD AN INTERIM REPAIR ABOVE LONGERON 16R. INSTALLED NEW SHEAR TIE SRM 51-01. (M)Jun 1, 2000 · N286AA · Doug DC982SDR TWAA0008709Intercostal · crackedDURING OP 16 MAINT CHECK, NUMBER 2 PYLON INTERCOSTAL WAS CRACKED OFF TOP 6 INCHES FROM FUSELAGE, BOTTOM AFT OF PYLON INTERIOR, AFT END. REMOVED CRACKED INTERCOSTAL. FABRICATED REPAIR PER SRM 53-01 PAGE 8. HEAT TREATED REPAIR DOUBLER 2024, 0.050 TO 2024-T3 PMay 24, 2000 · N921L · Doug DC932SDR TWAA0008708Intercostal · crackedDURING OP 16 MAINT CHECK ON RT PYLON BOTTOM AFT INTERIOR, 11 INCHES FROM FUSELAGE, TOP FWD INTERCOSTAL WAS CRACKED APPROX 2 INCHES LONG. CUT OUT CRACKED AREA, INSTALLED DOUBLERS PER SRM 54-01, PAGE 7 EXAMPLE D.May 24, 2000 · N921L · Doug DC932SDR QXEA0001567Bracket · crackedYYC- NR 2 ENGINE STUB WING WIRE/CABLE LOOM BRACKET BELOW PANEL O2D IS CRACKED. REPAIRED IAW FOKKER SRM 4-20-11 FIGURE 2 AND 51-31-01.May 23, 2000 · N480AU · Fokker F28MK4000SDR TWAA0008710Angle · crackedDURING OP 16 MAINT CHECK ON NUMBER 2 PYLON, TOP FWD CLIP ANGLE WAS CRACKED OFF ON INTERCOSTAL 3.5 INCHES FROM FUSELAGE AFT BOTTOM AREA. REMOVED BRACKET PER MO 72J95 AND PER REWORK DRAWING 5917717.May 23, 2000 · N921L · Doug DC932SDR C2XA00IA136Stiffener · dentedIAH - DURING C-CHECK INSPECTION, THE NR 1 ENGINE UPPER COWLING Z SECTION STIFFENER WAS FOUND TO BE DENTED. MAINTENANCE PERFORMED A DOUBLER REPAIR ON THE AFFECTED SECTION OF STIFFENER IAW EMB145 SRM 54-10-03, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICEMay 21, 2000 · N14960 · Emb EMB145SDR L1GA200000140Stiffener · crackedCRACKED LT PYLON VERTICAL STIFFENER.May 18, 2000 · N17533 · Doug DC932SDR TWAA0007705Intercostal · crackedDURING OP 16 MAINT CHECK ON NUMBER 2 PYLON, FOUND INTERCOSTAL CRACKED 3.5 INCHES FROM FUSELAGE AND 7 INCHES FROM FRONT, BOTTOM AFT AREA OF PYLON. REPAIRED CRACK PER SRM 54-01 PAGE 97 EX D. INSTALLED FASTENERS PER 51-30 AND 51-10-4. SEALED PER 51-70-2.May 10, 2000 · N921L · Doug DC932SDR MWEA00425Structure · crackedLEFT ENGINE PYLON BOX AREA DIVIDER CRACKED THRU RIVET HOLES AFT OF THE AFT SPAR BOTTOM ATTACH AREA. STOP DRILLED CRACK. FABRICATED AND INSTALLED REPAIR ANGLES.May 9, 2000 · N900ME · Doug DC915SDR TWAA0006906Angle · crackedDURING OP 16 MAINT CHECK, FOUND ON LT PYLON, ANGLE CRACKED BELOW FWD UPPER PYLON COWL LATCH. FABRICATED NEW ANGLE PER SRM 54-10-0, PAGE 5 FIGURE 3 ITEM 21, AND DOUGLAS DRAWING 5910308. TREATED PART PER SRM 51-10-3. REPLACED PART PER SRM 6-70-01.Apr 29, 2000 · N984Z · Doug DC931SDR MWEA00349Angle · crackedLEFT PYLON TO FUSELAGE ATTACH ANGLE (UPPER) IS CRACKED 10 INCHES FROM AFT EDGE. FABRICATED AND INSTALLED ANGLES AND HI-LOKS.Apr 21, 2000 · N810ME · Doug DC981SDR RRXA001774Panel · crackedDURING A MAINTENANCE VISIT, FOUND A 2 1/2 INCH CRACK ON THE RT WING IB SLOT PANEL, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED AND INSTALLED NEW PANEL IAW DC-8 SRM 51-3-0 AND DC-8 MM 27-80-1.Apr 20, 2000 · N961R · Doug DC873FSDR F3LA00045Channel · crackedDEN - DURING C-7 CHECK INSPECTION, REPORTED 1.6 INCH CRACKED IN RIGHT ENGINE INBOARD FIXED COWL AT LAST RIB, UPPER CROSS U-CHANNEL. MAINTENANCE FABRICATED REPLACEMENT U-CHANNEL, SHIMS AND CORNER BRACE PER SRM 54-10-2. (M)Apr 18, 2000 · N271FL · Boeing 7372L9SDR F3LA00058Structure · damagedDEN - DURING C-7 CHECK INSPECTION REPORTED A HOLE IN THE NR 2 ENGIEN INLET. MAINTENANCE REMOVED DAMAGED AREA. FABRICATED REPLACEMENT PARTS AND REPAIRED PER SRM 51-30-2. (M)Apr 17, 2000 · N271FL · Boeing 7372L9SDR F3LA00041Flange · crackedDEN - DURING C-7 CHECK INSPECTION, REPORTED 1 INCH CRACK IN U FLANGE AT LOWER MOUNT OF LT INBOARD FIXED COWL. MAINTENANCE FABRICATED U FLANGE AND DOUBLER AND REPAIRED PER SRM 54-10-01, 54-10-02, AND 54-10-03. (M)Apr 11, 2000 · N271FL · Boeing 7372L9SDR F3LA00040Cowling · crackedDEN - DURING C-7 CHECK INSPECTION REPORTED CRACK AT AFT UPPER END OF ENGINE INBOARD FIXED COWL IN FRAME APPROXIMATELY 12 INCHES FROM AFT END. THERE IS ALSO ANOTHER CRACK IN SAME FRAME APPROXIMATELY 1.2 INCHES LONG, APPROXIMATELY 6 INCHES FROM AFT END. ALSO AApr 11, 2000 · N271FL · Boeing 7372L9
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