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 P5CA9701327Spar Chord · corrodedLEVEL 1 CORROSION, NR 1 PYLON INBD AND OUTBD MID SPAR CHORDS HAVE LIGHT SURFACE CORROSION AT NAC ST 253.9-261 AT WL 181 ON UPPER AND LOWER SURFACE OF CHORDS. REMOVED CORROSION PER BOEING SRM 51-10-01 REWORKED AREA REPROTECTED IAW SRM 51-10-02, NON ROUTINE WORSDR P5CA9701228Spar Chord · corrodedLEVEL 1 CORROSION NR 4 PYLON I/B AND O/B MID SPAR CHORDS HAVE LIGHT SURFACE AT NAC ST 267 TO 257 ON UPPER AND LOWER SURFACE WL 180. REMOVED CORROSION PER BOEING SRM 51-10-01 AND TREATED PER SRM 51-10-02. SB/EO: NR 747-54-2159.SDR P5CA9701227Spar Chord · corrodedLEVEL 1 CORROSION NR 1 PYLON MID SPAR CHORDS I/B AND O/B HAVE LIGHT SURFACE ON UPPER AND LOWER SURFACE FROM NAC ST 253.9-261. REMOVED CORROSION PER BOEING SRM 51-10-01 AND TREATED PER SRM 51-10-02. SB/EO: NR 747-54A-2159.SDR P5CA9701184Brace · damagedNR 1 PYLON I/B DIAGONAL BRACE CHAFED FWD END. INSP AREA PER BOEING SRM 54-40-01 ZONE 3 FOUND TO BE WITHIN LIMITS, EDDY CURRENT C/W, NO CRACKS FOUND PER NDT 54-40-07 PART 6. BLENDED OUT AREA, FLAT PEENED AREA, TREATED AND PAINTED PER BOEING SRM 51-10-01 AND 5SDR P5CA9701183Brace · damagedNR 1 PYLON O/B DIAGONAL BRACE CHAFED FWD END. INSP AREA PER BOEING SRM 54-40-01 ZONE 3 TO BE WITHIN LIMITS, EDDY CURRENT C/W, NO CRACKS FOUND PER NDT 50-40-07 PART 6. BLENDED OUT AREA, FLAT PEENED AREA, TREATED AND PAINTED AS PER BOEING SRM 51-10-01 AND 54-4SDR P5CA9701182Bracket · damagedNR 4 PYLON RT SIDE DIAGONAL BRACE CHAFE MARK FROM 1ST STUD BRACKET. INSP AREA FOUND OK FOR SERVICE PER BOEING SRM 54-40-01, ZONE 3 EDDY CURRENT C/W PER NDT 54-40-04 PART 6, NO CRACKS NOTED. BLENDED OUT AREA, FLAT PEENED AREA, TREATED AND PAINTED AS PER BOEINSDR MWEA97566Angle · crackedDURING D-CHECK, FOUND CRACKS ON EXTERIOR SKIN ENGINE PYLON TO FUSELAGE ANGLE AT STATION 1019 RIGHT AND 1019 LEFT SIDE. MTC REPAIRED IAW SRM 54-04 FIG 10.SDR 9712789941Spar · failedDURING PREFLIGHT INSPECTION, FOUND THE RIGHT ENGINE SAGGING. FURTHER INVESTIGATION REVEALED THE RIGHT PYLON REAR SPAR UPPER CAP FAILED. REPLACED RIGHT REAR UPPER SPAR CAP AND FAIL-SAFE STRAP PER EA 99-113863.SDR MWEA97556Angle · crackedDURING C-CHECK, STA 1005 LT PYLON UP ATTACH ANGLE CRACKED IN RADIUS. MAINT REPAIRED IAW SRM 54-04 FIG 10 SHT 3.SDR P5CA9701178Door · damagedNR 2 PYLON OUTBOARD SAIL PLANE DOOR INSIDE SURFACE HAS PUNCTURE. REMOVED DAMAGED AREA AND HOT BONDED NEW DOUBLER IN PLACE IAW BOEING SRM 51-40-06.SDR P5CA9701177Flange · crackedNR 4 PYLON I/B SIDE AFT LWR ACCESS DOOR FLANGE CRACKED. BLENDED AREA TO REMOVE CRACK CONDITION IAW BOEING SRM 54-10-03 AND HFEC INSP IAW NDT PT-6 51-00-00 FIG 4.SDR P5CA9701125Brace · damagedNR 3 ENG PYLON DIAGONAL BRACE DAMAGED AND CHAFING ON O/B SAIL PLANE DOOR AT LOWER O/B SIDE. BLENDED OUT CHAFED AREA IAW BOEING SRM 54-40-01 FIG 5 MATERIAL WITHIN LIMITS.SDR P5CA9701124Brace · damagedNR 4 ENG PYLON DIAGONAL BRACE DAMAGED AND CHAFING ON O/B SAIL PLANE DOOR LOWER O/B SIDE. BLENDED OUT CHAFED AREA IAW BOEING SRM 54-40-01 FIG 5 MATERIAL WITHIN LIMITS.SDR WRLADRC0172Fairing · crackedNR 1 ENGINE PYLON AFT LOWER FAIRING, LEFT UPPER FORWARD CORNER CRACKED. TRIMMED AND DOUBLER REPAIR CARRIED OUT AS PER EN 559-97. (M)SDR CALA9701084Web · elongated holesINSPECTION FOUND SEVERAL ELONGATED FASTENER HOLES IN NR 3 PYLON FRONT SPAR WEB. THE WEB WAS REMOVED, A NEW WEB WAS FABRICATED AND INSTALLED IAW EA 5410-01109 AND SRM 51-30-00.SDR P5CA9701084Brace · delaminatedNR 3 PYLON DIAGONAL BRACE AFT SECTION DEEP CHAFE MARK FOUND EXCEED SRM 54-40-01, REF BOEING TELEX PAO-HKG-97-0009RE FOR REPAIR.SDR P5CA9701083Angle · delaminatedNR 4 PYLON FWD ENG MOUNT BHD CHAFE MARK FOUND ON I/B RADIUS ANGLE LWR SECTION. ORIGINAL THICKNESS 0.059 REMAIN 0.046 REF BOEING TELEX PAO - HKG- 97 - 0014RE FOR REPAIR.SDR P5CA9700839Rivets · shearedNR 4 PYLON TORQUE B/HEAD STIFFENER RIVETS FOUND SHEARED. REPLACED AND DETAILED INSP AT SURROUNDING STRUCTURE CARRIED OUT NIL FURTHER DAMAGE FOUND, REF NR 867322.SDR P5CA9700845Fairing · crackedNR 4 PYLON TO WING GLOVE FAIRING FOUND CRACKED AND TORN. REPAIRED CARRIED OUT IAW SRM 51-40-15, REF NR 860341.SDR P2EA97056Doubler · tornPAE - FOUND C-CHECK MAINTENANCE VISIT, NR 1 ENGINE SLIPPER FAIRING OUTBOARD LATCH DOUBLER TORN. REMOVED AND REPLACED LATCH DOUBLER AND FILLER PER SRM 54-30-2. (M)SDR P2EA97055Fairing · crackedPAE - FOUND C-CHECK MAINTENANCE VISIT, NR 1 ENGINE SLIPPER FAIRING NR 4 AND NR 5 RIBS ARE CRACKED AT OUTBOARD LATCH ATTACH POINT. REMOVED AND REPLACED NR 4 AND NR 5 RIBS ON NR 1 ENGINE SLIPPER FAIRING IAW 51-10-3. (M)SDR P5CA9700552Brace · damagedNR 3 ENG DIAGONAL BRACE CHAFED FWD END BOTH LT AND RT SIDES. INSPECTED ARE PER SRM 54-40-01 FOUND TO BE WITHIN LIMITS PER ZONE 2, BLENDED AREA PER SRM 54-40-01 C/W EDDY CURRENT OK FOR SERVICE PER NDT MM 51-00-00, SHOT PEENED, TREATED AND PAINTED PER SRM 54-40SDR P5CA9700551Brace · damagedNR 2 ENG DIAGONAL BRACE CHAFED FWD END BOTH LT AND RT SIDES. INSPECTED AREA PER SRM 54-40-01 FOUND TO BE WITHIN LIMITS PER ZONE 2, BLENDED AREA PER SRM 54-40-01 C/W EDDY CURRENT INSP NDT MM 51-00-00 OK FOR SERVICE, SHOT PEENED, TREATED AND PAINTED PER SRM 51-SDR P5CA9700550Brace · damagedNR 4 ENG DIAGONAL BRACE CHAFED AT FWD END LT AND RT SIDES. INSPECTED AREA PER SRM 54-40-01, FOUND TO BE WITHIN LIMITS PER ZONE 2 C/W EDDY CURRENT INSP PER NDT MM 51-00-00, FOUND OK FOR SERVICE PLUS BLENDED, SHOT PEENED, TREATED AND PAINTED PER SRM 54-40-01.SDR P5CA9700549Brace · damagedNR 1 ENG DIAGONAL BRACE CHAFED FWD END LT SIDE. INSPECTED AREA PER SRM 54-40-01, FOUND TO BE WITHIN LIMIT PER ZONE 2 AND 3. BLENDED AREA, EDDY CURRENT INSP C/W PER NDT MM 51-00-00 OK FOR SERVICE SHOT PEENED, TREATED AND PAINTED PER SRM 54-40-01.SDR 97ZZZM843Shear Pin · rustedNR 1 PYLON INBOARD SHEAR LINK PIN IS RUSTY, BOLT HAS BEEN REMOVED. REPLACED NR 1 PYLON INBOARD SHEAR LINK PIN IAW BAE DRAWING HC574H0030. (M)SDR P5CA9700529Seal Depressor · chafedNR 2 PYLON SAILBOAT INBOARD SIDE CHAFING DIAGONAL BRACE ON FORWARD END OF THE BRACE AND DOOR LIP. TRIMMED 1 RADIUS IN SEAL DEPRESSOR, CHECKED CHAFING OK PER BOEING SRM 51-40-01, EDDY CURRENT CHECKED PER NDT MANUAL 51-00-00 RESTORED FINISH.SDR P5CA9700528Fairing · crackedCRACK NR 3 ENGINE DOGHOUSE JUST AFT OF LEADING EDGE 2 INCHES LONG. REPAIRED PER BOEING SRM 54-50-03.SDR P5CA9700862Seal Fairing · crackedNR 4 PYLON UPPER FWD SLOT SEAL FAIRING IS CRACKED AT RT FWD CORNER. REPAIRED PER BOEING SRM 51-40-03.SDR P5CA9700861Seal · delaminatedNR 4 ENG SLOT SEAL IS SPLIT. REPLACED SEAL PER AMM 54-51-00.SDR P5CA9700860Seal · delaminatedNR 3 PYLON SLOT SEAL IS SPLIT. REPLACED PER AMM 54-51-00.SDR P2EA97057Rib · chafedPAE - FOUND C-CHECK MAINTENANCE VISIT, NR 1 ENGINE LEFT FORWARD COWL, NR 1 RIB IS CHAFED. CHAFED RIB IS OUT OF LIMIT PER SRM 54-10-1. REMOVED AND REPLACED NR 1 RIB PER SRM 51-30-2 AND 51-10-2. (M)SDR P2EA97051Bracket · crackedPAE - FOUND C-CHECK MAINTENANCE VISIT, NR 2 ENGINE OUTBOARD FORWARD COWL, FORWARD HORIZ LATCH ATTACH BRACKET IS CRACKED. REMOVED NR 2 ENGINE OUTBOARD FORWARD HORIZ LATCH ATTACH BRACKET, FABRICATED, TREATED, INSTALLED NEW ATTACH BRACKET IAW SRM 54-10-1. (M)SDR P5CA9701145Brace · chafedDEEP CHAFE MARK ON NR 3 DIAGONAL BRACE. REP 0-1R OF BLEND OUT CARRIED OUT IAW BOEING FAX S/N 206-266-6878, REF CWS NR 867323, 867324. ALSO RS R54-54-33401.SDR P5CA9700792Bracket · crackedNR 1 PYLON O/B SAIL FAIRING DOOR THE 5TH LATCH AFT ATTACH AND BRACKET. REPAIRED NR 5 LATCH PER BOEING SRM 51-10-01, IAW MM 54-32-00, REF NR 854014.SDR P5CA9700786Bracket · crackedCRACKED BRACKET NR 2 PYLON RT STRUT DOOR MOST AFT LATCH FITTING. REPLACED BRACKET IAW BOEING SRM 51-10-01, REF NR 854048.SDR P5CA9700784Bracket · crackedCRACKED BRACKET AT NAC 180 LOWER HOR FIRE WALL, METAL SEAL ATT ON LT AND RT SIDE. REPLACED BRACKET PER BOEING SRM 51-10-01.SDR P5CA9700783Rib · crackedCRACKED NR 2 PYLON RT SIDE RIB AT NAC 230, ACCESS FROM NR 483GL. REPAIRED CARRIED OUT IAW BOEING SRM 54-10-03, REF NR 854454 AND PROCESS SHEET S/N 240206.SDR P5CA9701008Pan · delaminatedNR 2 PYLON SLOT SEAL FWD UPPER PAN IS DELAMINATED AT NUMEROUS PLACES. REPAIRED IAW BOEING SRM 54-54-03, REF CWS NR 854125.SDR P5CA9701007Fairing · crackedNR 2 PYLON FWD FAIRING O/B BOTTOM INNER RUB STRIP IS TORN AND ATTACH ANGLE IS CRACKED. REPLACED RUB STRIP IAW BOEING SRM 51-10-01 REF CWS NR 867283.SDR CKSA97208Web · crackedDURING C-2 CHECK INSPECTION, FOUND NAC WEB AT NAC WL 181.6, NAC STA 246 AT DUCT ATTACH HOLE HAS SEVERAL CRACKS ON EDGE OF HOLE. REPAIRED WEB AS PER AIA ENGINEERING DRAWING AIA/E/2555. C-CHECK WORK CARD NUMBER 7TK7198. NON-ROUTINE TASK CARD NR 102153.SDR P2EA97046Web · wornPAE - FOUND C-CHECK MAINTENANCE VISIT, NR 1 ENGINE FORWARD WEB OF PYLON WORN THROUGH FROM SLIPPER FAIRING. REMOVED FORWARD WEB AND REPLACED WITH NEW WEB PER SRM 51-30-02 ON NR 1 ENGINE PYLON. (M)SDR EIAA970135Angle · crackedHKG - DURING C5/D CHECK INSPECTION, DISCOVERED NR 2 PYLON NAC STATION 221 FORWARD FACE RADIUS ANGLE IS CRACKED PAST STOP DRILL HOLE. REPAIR ACCOMPLISHED IAW SRM 54-10-03 FIGURE 19 AND SB 54-2042. (M)SDR UPS97823134Web · crackedINSPECTION TYPE:C, NR 1 PYLON O/B SIDE AT FWD ACCESS PANEL, PYLON WEB HAS A 3 INCH CRACK. AREA WAS MAPPED AND SUBMITTED TO ENRG ON N/R 634322. FABRICATED AND INSTALLED REPAIR DOUBLER IAW DHC SK-779-322 (REF UPS ENRG FILE NR DC8-54-0038).SDR P5CA9700522Skirt · damageNR 1 PYLON I/B SIDE, PYLON SKIRT AFT END DAMAGED. CLEANED UP DAMAGED AREA, FABRICATED REPAIR DOUBLER, FILLER AND INSTALLED THE SAME PER BOEING SRM 54-34-03.SDR ABXA9700982Angle · crackedDURING C-CHECK, FOUND NR 2 PYLON UPPER FUSELAGE ATTACH ANGLE AT F/STA 1038 CRACKED. STOP DRILLED AND REPAIRED IAW DC9 SRM 50-04, FIGURE 10.SDR ABXA9700971Angle · crackedDURING C-CHECK, FOUND NR 1 PYLON LOWER OUTBOARD ANGLE CRACKED FORWARD OF AFT ENGINE MOUNT. REPAIRED IAW ABX REA D954-19336.SDR 9710015503Web · crackedDURING L-CHECK, FOUND CRACK IN NR 2 PYLON SIDE WEB AT CUTOUT FOR CROSS BRACE APPROXIMATELY NACELLE STA 125. REPAIRED PER EA 55-150276.SDR ABXA9700969Web · crackedDURING C-CHECK, FOUND NR 1 PYLON OUTBOARD WEB CRACKED AT LOWER ATTACH ANGLE FORWARD OF AFT ENGINE MOUNT. REPLACED WEB (P/N 9958221-3) IAW DC9 SRM 51-30-2 AND 51-30-5.SDR ABXA9700963Angle · crackedDURING C-CHECK, FOUND ATTACH ANGLE CRACKED INSIDE OF NR 1 PYLON UPPER OUTBOARD CORNER INSIDE PANEL 8105A. REPLACED ANGLE (P/N 9958154-9) AND FITTING (P/N 4919864-1) IAW DC9 SRM 51-30-1, 51-30-2 AND 51-10-4.
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