JASC 5410
Service difficulty reports · 4,119
Reports filed under 5410 · Nacelle/Pylon, Main Frame, 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 = '5410' 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 = '5410' 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 QXEA200301090Structure · crackedTOP OUTBOARD FASTENER HOLE FOR REFUEL/DEFUEL SHUTTOFF VAVLE IS CRACKED. REPAIRED IAW DHC-8 SRM 51-00-06 AND RD 8-54-1839.SDR UIEA200300051Fitting · damagedDURING C-CHECK, NR 1 PYLON OB SPRING BEAM SHEAR TRANSFER FITTINGS FOUND DAMAGED DUE TO CONTACT WITH SPRING BEAM. CONTRACT RESULTED FROM MISLOCATION OF FITTINGS. SUBJECT FITTINGS WERE TRIMMED TO REMOVED DAMAGE, NDT INSPECTED, & RESTORED PER DRAWING. FITTINGSSDR QXEA200300982Support Angle · crackedNR 2 ENGINE LOWER NACELLE UPPER DECK SUPPORT ANGLE IS CRACKED. REPAIRED IAW Q400 RD 8/4-71-016.SDR AWXA200301051Angle · crackedDURING C-16 CHECK A 1 1/8 INCH CRACK WAS FOUND ON NR 1 ENGINE RT FORWARD COWL LOWER ZEE ANGLE AT RIB 7, NAC STA 151. MAINTENANCE CUTOUT CRACK ON RIB 7; FABRICATED A REPAIR DOUBLER; INSTALLED REPAIR PART IAW B737-200 SRM 54-40-03, FIG. 001.SDR GTIA030665Attach Angle · crackedFTW - FOUND RT ENGINE UPPER PYLON ATTACH ANGLE CRACKED AT CANT 1500. CUT OUT DAMAGED CRACK. FABRICATED ANGLE DOUBLER AND FILLER. INSTALLED DOUBLER AND FILLER REPAIR. (M)SDR CA030807003Cowling · damaged(CAN) CREW WAS NOTIFIED BY TOWER THAT THE LT UPPER ENGINE COWLING HAD COME OFF THE AIRCRAFT, AND WAS LAYING ON THE RUNWAY. A/C RETURNED AND LANDED THEY FOUND THE FASTENER STILL LOCKED ON THEIR DZEUS RECEPATCLE .THEY REPLACED THE DAMAGED DZEUS RECEPTACLE AND RESDR C2XA03SH236Stiffener · gougedDURING C-CHECK, THE NUMBER 1 UPPER ENGINE COWLING INTERNAL STIFFENER WAS FOUND TO BE GOUGED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED STIFFENER IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA03SH232Stiffener · gougedDURING C-CHECK, THE NUMBER 2 LOWER COWLING INTERNAL STIFFENER WAS FOUND TO BE GOUGED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED STIFFENER IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA03SH231Stiffener · damagedDURING C-CHECK THE LEFT HAND UPPER COWLING INTERNAL STIFFENER WAS FOUND TO BE DAMAGED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED STIFFENER IAW EMB 145 SRM 54-10-01. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR QXEA200300830Support Fitting · loosePDX - LOWER INBOARD ENGINE SUPPORT FITTING IN NACELLE IS PULLED LOOSE FROM LOWER BOX STRUCTURE OF NACELLE. REPAIRED IAW Q400 SRM 51-25-15, PAGE 205-G-1-4 AND SRM 51-40-15, PAGE 203.SDR C2XA03SH221Stiffener · gougedDURING C-CHECK, THE LEFT HAND LOWER COWLING INTERNAL STIFFENER WAS FOUND TO BE GOUGED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 54-10-07. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA03SH220Stiffener · gougedDURING C-CHECK, THE RIGHT HAND UPPER COWLING INTERNAL AFT STIFFENER WAS FOUND TO BE GOUGED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED STIFFENER IAW EMB 145 SRM 54-10-01. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA03SH219Stiffener · gougedDURING C-CHECK, THE LEFT HAND UPPER COWLING INTERNAL AFT STIFFENER WAS FOUND TO BE GOUGED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 54-10-07. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA03SH218Stiffener · gougedDURING C-CHECK, THE LEFT HAND LOWER COWLING INTERNAL AFT STIFFENER WAS FOUND TO BE GOUGED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED STIFFENER IAW EMB 145 SRM 51-40-03. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR DHL2003746009Fire Seal · unsecure1) NR 1 FIRE FAULT LOOP LIGHT ILLUMINATED. 2) FOUND NR 1 ENGINE FIRE LOOP UNSECURED NEXT TO FCU. RESECURED FIRE LOOP AND OPS CHECKED SERVICEABLE IAW M/M 26-11-00.SDR C2XA03SH214Stiffener · gougedDURING C-CHECK, THE LEFT HAND LOWER COWLING INTERNAL STIFFENER WAS FOUND TO GOUGED AT FRAME 71L. MAINTENANCE REMOVED AND REPLACED THE AFFECTED STIFFENER IAW EMB 145 SRM 51-40-03. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR 0301516717Frame · crackedDURING "L" CHECK FOUND CRACK IN BULKHEAD NR 1 PYLON FRAME WEB. REPAIRED PER EA 67-165077.SDR QXEA200300789Strut · gougedPDX - A CIRCULAR GOUGE EXISTS IN THE INBOARD CENTER DIAGONAL STRUT. REPAIRED IAW HORIZON AIR EA 6-54-263.SDR DL757030561Fitting · corrodedDURING THE ACCOMPLISHMENT OF SIP MODIFICATION, CORROSION WAS FOUND ON THE UPPER SURFACE OF THE LT DOUBLER OF THE MID SPAR INSTALLATION. REPAIRED PER: ER/A 385115-14AD.SDR QXEA200300773Bracket · crackedINSIDE OF LOWER NACELLE LEFT HAND LOWER AFT CONE BRACKET CRACKED. REPAIRED IAW RD 8/4-71-016.SDR QXEA200300750Strut · chafedPDX - CHAFING ON LOWER SUPPORT STRUT NR 2 ENGINE. REPAIRED IAW RD 8-54-036.SDR QXEA200300749Strut · gougedPDX-GOUGED UPPER SUPPORT STRUT AFT AREA OUTBOARD NR 2 ENGINE. REPAIRED IAW RD8-54-1811, RD8-54-036 AND HORIZON AIR EA 2-54-172.SDR HEEA087832Door · corrodedINTAKE COWLING DOOR IS CORRODED AND CHAFED BEYOND LIMITS. REPLACED WITH SERVICEABLE PART.SDR C2XA03SH179Structure · chafedDURING C-CHECK THE NUMBER ONE UPPER COWLING AFT EDGE MEMBER WAS FOUND CHAFED. MAINTENANCE REMOVED AND REPLACED AFFECTED MEMBER IAW EMB 145 SRM 54-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.SDR ABXA030192Strut · gougedDURING INSPECTION, TWO GOUGES WERE FOUND ON NR 2 ENGINE STRUT RIGHT SKIN PANEL NEAR ACCESS DOOR CUT OUT. MAXIMUM DEPTH OF BLENDED OUT REQUIRED TO COMPLETELY REMOVE DAMAGE, 0.025 INCH. REPAIRED AREA IAW REA .SDR 03FDEA00855Bolt · looseREF EO 8-5410-7-3321 ITEM A 1 AND 2 GAIN ACCESS TO NR 1 PYLON AFT BULKHEAD REAR BOLTS, 5 OF THEM FOUND LOOSE. EO 8-5410-7-3321 BOLTS WERE INSPECTED AND HOLES CHECKED BY NDT DEPT. BOLTS RETORQUED AND AREA PREP FOR CLOSING.SDR AC2A087919Latch · brokenRT FWD ENGINE COWL LATCH FAILED IN FLIGHT. UPON LANDING IT WAS DISCOVERED THAT THE COWLING HAD LIFTED 2 INCHES ON RIGHT HAND SIDE. THE LATCH HOOK ON THE FWD. LATCH WAS COMPLETELY MISSING AND THE AFT LATCH WAS CLOSED BUT NOT HOOKED TO THE AIRFRAME FITTING. FWD.SDR USAASA03057Panel · looseEN ROUTE SFO-PIT, ON TAKEOFF, A LOUD AIR NOISE FROM LEFT SIDE OF AIRCRAFT WAS HEARD, FOLLOWED BY FIVE COMPRESSOR STALLS. NO IRREGULAR ENGINE INDICATIONS WERE NOTED. CREW FOLLOWED THE QUICK REFERENCE HANDBOOK PROCEDURES. BOTH ENGINES REMAINED IN OPERATION THSDR 03FDEA00816Spar · damagedCOMPLY WITH E.A.6-5455-70907 PYLON- REPAIR OF FWD FAIRING UPPER SPAR ANGLE 9333M29P112A. FACT 27MAY03 11:32 BFM U WORK COMPLIED WITH IAW/E.A. 6-5455-70907, PYLON-REPAIR OF FWD FAIRING UPPER SPAR ANGLE 9333M29P112A.IAW/51-70-40-FIG 201.SDR 03FDEA00800Rib · crackedNR 855 NR 3 ENGINE RTCORE COWL FWD RIB CRACKED AT UPPER L/E RADIUS. CLOSING ACTION ON 05/24/03. REMOVED FASTENERS FOR ACCESS IAW SRM 51-31-01. WELLED CRACK ON MAE TRAVELER T2/336399 IAW SRM 54-31-01. REINSTALLED FASTNERS IAW SRM 51-35-01, PAINTED TEFLOSDR 03FDEA00759Door · damagedNR 1 ENGINE RT T/R COWL BLOW OUT DOOR INTERIOR HAS TWO EACH CHAFED AREAS WHERE RETAINING CABLE HAS MADE CONTACT. REPAIRED DAMAGED AREAS BY BLENDING, ALODINING, AND FILLING AREA WITH HIGH TEMP SEALANT, AND APPLYING A COAT OF TEFLON PAINT IN THE REWORKED SDR C2XA03SH136Structure · gougedSHV DURING C-CHECK LEFT HAND ENGINE UPPER COWLING AFT EDGE MEMBER WAS FOUND TO HAVE RUB MARKS. MAINTENANCE REMOVED DAMAGE AND REPLACED AFFECTED MEMBER IAW EMB 145 SRM 54-10-01. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.SDR C2XA03SH133Stiffener · gougedSHV DURING C-CHECK, THE RIGHT HAND LOWER ENGINE COWLING HAS RUB MARKS ON THE MOST AFT INBOARD STIFFENER. MAINTENANCE REMOVED DAMAGE AND REPLACED AFFECTED STIFFENER IAW EMB 145 SRM 54-10-07. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.SDR ASAA0310466Structure · dentedOKC - DURING C-CHECK, FOUND NR 1 ENGINE PYLON AT WING STATION 191 DENTED. REMOVED DAMAGED AREA AND REPAIRED PER EA. (M)SDR 03FDEA00696Plate · crackedNR 3 ENGINE O/B T/R TRANSILATING COWL UPPER SLEVE WALL PANEL CRACKED. REMOVED SIDEWALL PANEL PLATE IAW SRM 51-35-01. RECEIVED NEW PART ON TRAVELER T2/331654, LOCATED AND DRILLED HOLES IAW SRM 51-35-01, PRIMED IAW SRM 51-21-01, INSTALLED PLATE IAW SRM 51-35-0SDR AUS20030476Fairing · missing(AUS) NR 2 ENGINE TRANSFER DRIVE FAIRING MISSING. DAMAGE TO BLOCKERDOORS AND FLAPS.SDR 03FDEA00653Pylon · damagedNR 1 ENGINE PYLON HAS I/B CENTER SECTION AT CENTER T/R HINGE POINT BOWED INWARD APPROX 17 INCHES HIGH AND 20 INCHES LONG WITH 1 INCH DEPTH. SUBSEQUENT DISASSEMBLY AND INSPECTION REVEALED, I/B SIDE OF SKIN AT RIB 7 HAD DEFORMED GUSSET, PYLON PLANK FROM RIB 1 TSDR ASAA0380346Door · crackedOAK - FOUND DURING 15K CHECK, LEFT ENGINE NACELLE CRACKED ON UPPER DOOR. REPLACED DAMAGED SECTION ARE REPAINTED PER SRM 51-10 AND EA 5410-0054. (M)SDR 03FDEA00466Skin · chafedNR 3 ENGINE NACELLE SKIN CHAFED AROUND NR 4 INBOARD LATCH. *S/D* REPAIRED SKIN AT NR 4 LATCH IAW BOEING 727-200 SRM 54-10-03.SDR HNAA0300020Cone · brokenCREW REPORTED A WHISTLE SOUND FROM NR 1 ENGINE WHENEVER POWER WAS APPLIED. FOUND A PIECE OF THE NR 1 LOWER COWL AFT CONE HAD BROKEN OFF CAUSING FOD DAMAGE TO NR 1 ENGINE. REPLACED ENGINE AND LOWER COWL.SDR UPS03440602Frame · crackedINSPECTION TYPE: C, NR 2 PYLON REAR ENGINE MOUNT BULKHEAD AFT FRAME FOUND CRACKED AT 4 & 5 O/C POSITION ( LOOKING FORWARD ). NR 2 PYLON REAR ENGINE MOUNT BULKHEAD I/B AFT FRAME REPAIRED AS PER RS 54-53-35009 AND UPS REPAIR AUTHORIZATION 747-54-20035 INSPESDR UPS03440601Frame · crackedINSPECTION TYPE: C, NR 2 PYLON REAR ENGINE MOUNT BULKHEAD FORWARD FOUND CRACKED AT 7 O/C POSITION ( LOOKING FWD ). NR 2 PYLON REAR ENGINE MOUNT BULKHEAD O/B FORWARD FRAME REPAIRED AS PER RS 54-53-35009 AND UPS REPAIR 747-54-20035 REPEAT DVI AND HFEC INSPESDR QXEA0300482Brace · gougedFORWARD STABILIZER BRACE ASSEMBLY IS GOUGED IN TWO LOCATIONS ON LEFT HAND NACELLE. REPAIRED IAW Q400 AMM 32-11-16-400-801, PAGE 411, PARAGRAPH 4A.SDR 03FDEA00407Seal · gougedNR 3 ENGINE O/B CORE COWL UPPER SEAL AFT OF AFT HINGE GOUGED. CLOSING ACTION ON 04/07/03. REMOVED DAMAGED SEAL IAW SRM 51-35-01. FAB NEW SEAL ON TRAVELER T2/304970. INSTALLED SEAL IAW SRM 51-35-01.SDR 03FDEA00410Frame · gougedRIGHT PYLON UPPER PANEL 487EL, INNER FRAME GOUGED AND PREVIOUS REPAIR AND L/E CRACKED. CLOSING ACTION ON 04/07/03. REMOVED FRAME IAW SRM 51-35-01. FAB NEW FRAME WITH TRAVEER T2/324411. INSTALLED NEW FRAME IAW SRM 51-31-01 AND SRM 51-31-01.SDR GTIA030258Liner · damagedFOUND RT ENGINE INLET CASE ACOUSTIC LINER DAMAGED IN 4 PLACES. REPAIRED RIGHT ENGINE INLET AT DAMAGED AREAS. (M)SDR 03FDEA00389Pylon · damagedNR 1 ENGINE PYLON RIGHT SIDE CLOSE OUT ON LOWER WING BROKEN ABOVE PANEL 437ER. CLOSING ACTION ON 04/05/03. ON NR N00313. REMOVED CLOSE-OUT PANEL ROUTED TO FAB IAW SRM 51-31-01. T/R NR T2/322652 AND 1 PANEL ON T2/322695, LOCATED AND DRILLED IAW SRM 51-31-0SDR QXEA0300458Door · chafedRIGHT HAND NACELLE REFUEL/DEFUEL DOOR CHAFED ON INSIDE AT LIGHT SWITCH. REPAIRED IAW HORIZON AIR EA 6-54-225.SDR QXEA0300430Bracket · crackedPDX-NR 1 NACELLE FINGERNAIL DECKING AND SUPPORT BRACKET CRACKED AT AFT FINGERNAIL ATTACHMENT POINT. REPAIRED IAW RD8/4-54-033 AND RD8/4-54-044.SDR QXEA0300429Bracket · crackedPDX- NR 2 NACELLE FINGERNAIL DECKING AND SUPPORT BRACKET CRACKED AT AFT FINGERNAIL ATTACHMENT POINT. REPAIRED IAW RD8/4-54-033 AND RD8/4-54-044.
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