N942FD
Service difficulty reports · 147
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. 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 n_number = 'N942FD' AND registry_match = 'registration' 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 n_number = 'N942FD' AND registry_match = 'registration' 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 FDEA201608262993Screw · shearedAT 02:30 ZULU AFTER LENGTHY WEATHER DELAY, CAM ON OUTSIDE OPENING MECHANISM OF LT FORWARD ENTRY DOOR BROKEN. RELEASED FOR SERVICE IAW MEL: 52-11-01-A, CATEGORY-B, EXPIRATION : 29AUG16. MEL 52-11-01-A: L1 DOOR INOPERATIVE. INSPECTED DOOR, BEARING DOESN`T AFFESDR FDEA201607272635Window · out of adjustFO'S R2 WINDOW DIFFICULT TO LOCK REMOVED R2 WINDOW LINING AND DISCONNECTED WIRING IAW MM 56-11-02-4. PULLED & COLLARED R2 WINDOW HEAT CIRCUIT BREAKER P70 PANEL. ADJUSTED R2 WINDOW AND INSTALLED LINING IAW AMM 56-11-02-5-0. RESET R2 WINDOW HEAT CIRCUIT BRSDR FDEA201607082364Slat · damagedFIXED WING UNDER NR 5 LE SLAT HAS A HOLE CRACK. FURTHER INSPECTION FOUND DELAMINATION OF FIXED WING LE TO EXTEND TO ALL AREA UNDER THE MISSING TRAILING EDGE OF NR 5 SLAT. REPLACED SLAT AND MADE TEMP REPAIR TO LEADING EDGE. FERRY FLIGHT TO VQQ FOR PERMANENT SDR FDEA201607082342Slat · damagedNR 5 LE SLAT HAS 6 FT TRAILING EDGE MISSING. REMOVED AND REPLACED THE NR 5 LE SLAT ASSY IAW 27-81-01-4 AND EA F-5710-T0326621. OPS CHECKED GOOD.SDR FDEA201606091914Fitting · damagedNR 1 PYLON OTBD AFT TR FITTING LOWER AFT HOLE DAMAGED. COMPLIED WITH EA F-5450-T0325811 P1 OF NR 1 PYLON OB AFT TR FITTING LOWER AFT HOLE.SDR FDEA201606031799Frame · gougedFORWARD ACCESSORY BS 231 FRAME HAS A GOUGE. REPAIRED FWD ACCESSORY BS 231, FRAME IAW F-5310-T0325521 P1.SDR FDEA201606011780Skin · wornC1 DOOR CONTROL PANEL DOOR CUT OUT LOWER EDGE HAS DEEP WEAR MARK CTR AREA. REPAIRED C1 DOOR CONTROL PANEL DOOR CUT OUT LOWER EDGE IAW EA F-5330-T0325633, P1.SDR FDEA201601060054Clamp · looseRIGHT BLEED DUCT LEAK EICAS MSG AT FL 380. COMPLIED WITH QRH. ASSOCIATED STATUS MSG, DUCT LEAK LP, AFTER LANDING. TROUBLE SHOT IAW TSM 26-18 FAULT TREE 802, FAULT CODE 64. RT WING LE ALARM A & B. RESET CARD FILE IAW FIM, FOUND RT WING PNEUMATIC DUCT IN ISDR FDEA201503160938Unknown · malfunctionedON TAXI INTO GATE, PARKING BRAKE WOULD NOT SET. ACCOMPLISHED TEST OF THE PARKING BRAKE SYS IAW AMM 32-44-00-5. ALL CHECKED NORMAL, NO PREVIOUS HISTORY. OK FOR SERVICE.SDR FDEA201411163723Collar · damagedWHILE PERFORMING ACFT ORIENTATION, L1 DOOR GUST LOCK FAILED. REMOVED AND REPLACED THE L-1 DOOR HOLD OPEN LOCK COLLARSDR FDEA201410293415Strap · out of positionENTRY DOOR L1 WOULD NOT ARM. FOUND SMALL STRAND OF NYLON STRAP IN WAY OF GIRT BAR WHILE CLOSING. REMOVED & STOWED STRAP BACK IN POUCH & OPERATIONS CHECKED NORMAL. LIGHT ILLUMINATED NORMAL IAW AMM 52-11-25-5-0.SDR FDEA201405171066Skin · corrodedDURING INSPECTION, CORROSION WAS FOUND AT LAP SEAM APPROXIMATELY BS 1304, STRINGER 14R. REPAIRED IAW EA F-5330-T0308220 P1.SDR FDEA201405171065Skin · corrodedCORROSION CLOSE TO LAP SEAM AT BS 755 - 760, STRINGER 26R. REPAIRED IAW EA F-5330-T0308242 P1.SDR FDEA201305040912Gust Lock · brokenL1 DOOR GUST LOCK COLLAR BROKEN. R & R L1 DOOR GUST LOCK REF AMM 52-11-08-8. OK FOR SERVICE.SDR FDEA201212184363Guide Arm · brokenON ARRIVAL, FOUND R1 DOOR PARTIALLY CLOSED. UPON FUTHER INSPECTION FOUND ROD END ASSY BROKEN OFF OF ARM GUIDE, SAME MANUAL, FIG AND SHEET ITM 348. R & R GUIDE ARM ASSY IAW MM 52-11-04-2. INSTALLED SLIDE IAW MM 25-66-01-4. PERFORMED PRESSURE STOP ADJUSTMENSDR FDEA201211063862Valve · inoperativePARKING BRAKE TAKES EXCESSIVE AMOUNT OF PRESSURE TO REACH "DETENT". ACFT WILL STILL MOVE WITH "PARKING BRAKE" LIGHT ON EICAS. R & R THE PARK BRAKE VALVE.SDR FDEA201209093267Gust Lock · brokenL1 DOOR GUST LOCK BROKEN. REMOVED GUST LOCK IAW AMM 52-11-08-4. REASSEMBLED L1 DOOR HANDLE WITH REPLACED BEARINGS AND WITH NEW CENTER SHAFT, COLLAR REF MM 52-11-13 THROUGH NR 3. COMPLETED DOOR HANDLE MECHANISM ASSY, AND PERFORMED OPS CHECK IAW AMM 52-11-SDR FDEA201209073273Handle · unknownL1 DOOR WILL NOT CLOSE. L1 DOOR EXTERIOR HANDLE IS BROKEN, THE FLIPPER HANDLES WILL SPIN 360 DEGREES WITHOUT RESISTANCE. COMPLETED DOOR HANDLE MECHANISM ASSY AND PERFORMED OPS CHECKED IAW AMM 52-11-13-4, DOOR OPS CHECKED NORMAL.SDR FDEA201207162590Collar · brokenDURING PRE-DISPATCH CHECK, NOTED L1 DOOR HOLD OPEN LOCK COLLAR BROKEN. REMOVED BROKEN PIECES. REPLACED LOCKING COLLAR AND LATCHING MECHANISM ON L1 DOOR IAW MM 52-11-08-4, OPS CHECKED GOOD.SDR FDEA201207132575Mechanism · brokenDURING PRE-DISPATCH CHECK, NOTED L1 DOOR HOLD OPEN LOCK COLLAR BROKEN. REPLACED LOCKING COLLAR AND LATCHING MECHANISM ON L-1 DOOR IAW MM 52-11-08-4, OPS CHECKED GOOD IAW SAME.SDR FDEA201206212290Slide · dislodgedLEFT ENTRY DOOR WAS DISARMED. DOOR WAS CRACKED OPEN FROM INSIDE. PERSONNEL FROM THE OUTSIDE OPENED THE DOOR FURTHER, AT WHICH TIME IT APPEARED THE DOOR CAUGHT AND THE SLIDE FELL OUT. SLIDE DID NOT FULLY DEPLOY. STILL SHOWS GREEN PRESSURE ON THE SLIDE. WSDR FDEA201205211913Skin · damagedEXTERNAL LOWER FUSELAGE LAVATORY SERVICE PANEL CUT OUT EDGE DOUBLER AFT/INBD CORNER BUCKLED COMPLIED WITH EA F-5330-157269 FUSELAGE PLATES AND SKIN-SECTION 41-SKIN CORROSION. REPAIR STA 418-430 S-28L REF 8100-9 DATED MAY 17, 2012. MAJOR REPAIR.SDR FDEA201205151814Structure · crackedNR 2 PYLON, HORIZ FLANGE FASTENER HOLE CRACKED IN TITANIUM RT THIRD HOLE FROM AFT BULKHEAD. REAMED HOLE TO .405 IAW EA F-5450-157204 STEP1, AND 2ND HOLE TO .437 IAW EA F-5450-157204, STEP 3, NDT CHECK FOR CRACK, NO CRACK NOTED. INSTALLED FASTNER IAW-SRM-51-40SDR FDEA201205041736Bushing · migratedNR 2 PYLON MID SPAR ATTACH FITTING LUG RT SIDE BUSHING MIGRATED. (RT SIDE) ACFT SIDE. REMOVED MIGRATED BUSHING IAW SOPM-20-50-03. NO CORROSION NOTED, MEASURED LUG BORE AND IT IS 1.8140 FOUND TO BE OVERSIZE DIAMETER IAW DWG 112N7003, HFEC INSPECTED IAW NDTM SDR FDEA201204231526Skin · damagedFOUND SCRIBE LINE AT S14R LAP JOINT FROM BS 439.094 - 445.813. REPAIR ACCOMPLISHEDIAW EA F-5330-157266. MAJOR REPAIR.SDR FDEA201204121380Skin · damagedFOUND VERTICAL CUT ON SKIN PANEL AT BS 661 S26R, LEADING INTO BUTT JOINT, REMAINING ON LOWER SKIN SURFACE. ACCOMPLISHED EA F-5330-157270. "MAJOR REPAIR".SDR FDEA201204071286Skin · dentedFUSELAGE SKIN DENTED FWD OF AFT PRESSURE BULKHEAD BS 1720, S24-25R.SDR FDEA201204031241Stringer · gougedRIGHT UPPER LOBE OF R4 DOOR, STA 1681.8. GOUGED ALONG STRINGER 13R. COMPLIED WITH EA F-5310-157257. MAJOR REPAIR.SDR FDEA201203231085Skin · misrepairedFUSELAGE SKIN MISREPAIRED AT BS 760-780 BETWEEN S16-17L. REPAIRED ON STAM 47461010001 AND STAM EA 757- 5331-16 -F3678, REV. MAJOR REPAIR.SDR FDEA201203231084Skin · dentedLEFT LOWER EXTERNAL FUSELAGE AT BS 760 S18L DENTED. REPAIRED STAM 47461000001 AND STAM EA 757-5331-16-F3678. MAJOR REPAIR.SDR FDEA201203130925Panel · damagedNR 1 PYLON DOOR CUTOUT FOR DOOR PANEL 433LR HAS MISSING MATERIAL IN UPPER AFT CORNER. REPAIRED IAW EA F-5450-157272.SDR FDEA201203130920Skin · dentedSKIN AT BS 1871 AT S-21-L DENTED A=2.65 Y=.010 A/Y=265, DENT OUT OF LIMITS DUE TO AXIS ON STRINGER,IAW-SRM-53-00-01 FIG 101, DET III. ACCOMPLISHED EA F-5330-157262. CAT A, MAJOR REPAIR.SDR FDEA201203130919Panel · corrodedNR 2 PYLON CUTOUT FOR PANEL 443LL HAS CORROSION IN UPPER AFT CORNER. COMPLIED WITH EA F-5450-159901, CAT."A" MAJOR REPAIR.SDR FDEA201203130918Skin · misrepairedNR 2 PYLON OTBD SKIN HAS AN EXISTING REPAIR THAT EXCEEDS LIMITS OF SB 757-54-0022. R & R NR 2 PYLON OTBD SKIN IAW EA F-5450-159905. MAJOR REPAIR.SDR FDEA201203090850Skin · dentedSKIN AT BS 1862 S21L, DENTED. ACCOMPLISHED EA F-5330-157239. MAJOR REPAIR.SDR FDEA201203090856Floorbeam · corrodedBS 310, FLOORBEAM CAP CORRODED LBL 62-RBL 62. REMOVED CORROSION IAW-SRM-51-10-02, CHECKED LIMITS IAW-SRM-53-00-01 PG 101-103. DETAIL II AND III, ORIGINAL MAT THICKNESS .100, D=.027 L=1.1 W=1.3, FOUND TO BE OUT OF LIMITS. REMOVED FLOORBEAM UPPER TEE CAP, INSSDR FDEA201203050784Skin · corrodedCORROSION ON LOWER OUTSIDE SKIN BS 660 S26 - 30L. REMOVED CORROSION IAW SRM 51-10-02 ORIGINAL MATERIAL .063, REMAINING .052. FOUND OUT OF LIMITS IAW SRM 53-00-01 FIG 101 DETIAL II. REPAIRED IAW SRM 51-40-02. MAJOR REPAIRSDR FDEA201203050785Spar · corrodedLEFT WING REAR SPAR HAS CORROSION. BLEND LIMIT TOLERENCES HAVE BEEN EXCEEDED IAW EA F-2822-7-5009, PT3, STEP B1 ACCOMPLISHED EA F-5710-156998 STEPS 1 THRU 5.SDR FDEA201202290707Skin · damagedFOUND MULTIPLE TOOLING MARKS, FAIRING CONTACT AREA OF LAP SEAM AT S-20L BS 1326-1332. ACCOMPLISHED EA F-5330-157215. MAJOR REPAIR.SDR FDEA201202230674Skin · delaminatedLT INBD AFT T/E FLAP LOWER SKIN HAS PREVIOUS REPAIR THAT IS CRACKING. REPAIRED LT INBD AFT T/E FLAP LOWER SKIN IAW SRM 51-70-06. REF EA F-5750-157259 ISSUED FOR TRACKING-WINGS -FLIGHT SURFACES -EO F-5100-7-5001 LT INBD AFT FLAP-RSC REPAIR TRACKING. MAJOR RESDR FDEA201202220645Skin · misrepairedFUSELAGE SKIN BS 700 BETWEEN S24-26R MISREPAIRED. REPAIRED IAW EA F-5330-157216SDR FDEA201202220643Support Beam · corrodedNLG STRUCTURE UPPER SUPPORT BEAM STA 345 HAS CORROSION FWD AND AFT SIDES. REMOVED NLG UPPER SUPPORT BEAM IAW SRM 51-40-02 AT STA 345. COMPLIED WITH EA F-5310-157258. INSTALLED NLG UPPER SUPPORT BEAM IAW SRM 51-40-02. MAJOR REPAIR.SDR FDEA201202180613Skin · dentedEXTERNAL FUSELAGE SKIN BS 470 BETWEEN S21-22R DENTED. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-01, FIG 101 DETAIL III. REPAIRED DENT IAW SRM 53-00-01, FIG 201 REPAIR 3 REF SRM 53-00-01, FIG 201. REPAIR 17 NOTE "D" CATEGORY "B" MAJOR REPAIR.SDR FDEA201202150584Skin · misrepairedFUSELAGE SKIN BS 1720 TO 1726, S16 TO 17L MISREPAIRED. REPAIRED IAW EA F-5330-157000.SDR FDEA201202150583Beam · corrodedSTA 377 BL-0 NOSE WHEEL WELL UPPER TORQUE BOX BEAM CORRODED. REMOVED CORROSION AT STA 377 BL-0. FOUND TO BE OUT OF LIMITS IAW SRM 53-10-04, FIG 101 DETAIL IV, COMPLIED WITH EA F5310-157249. FUSELAGE MAIN FRAME - SECT 41 STA 377.5 NOSE WHEEL WELL TOP PANEL SDR FDEA201202140577Skin · misrepairedCARGO DOOR INNER SKIN MISREPAIRED. REPAIRED IAW SRM 51-70-13 FIG 1, & EA F5230-157271. MAJOR REPAIR.SDR FDEA201202130569Door Frame · corrodedL2 DOOR CUT OUT LOWER FWD FRAME INNER CHORD CORRODED. REMOVED CORROSION IAW SRM 51-10-02 BLENDED AREA MEASURES L= 3.0 W= 1.5 D= .018 ORIGINAL MATERIAL .080, .062 REMAINING. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-07 FIG 101 DETAIL II PG 103. REMOVED AND RSDR FDEA201202090537Skin · corrodedFOUND CORROSION ON LAP SEAM AT S20L, BS 1334.5. REPAIRED IAW EA F-5330-157215. MAJOR REPAIR.SDR FDEA201202030465Beam · corrodedNOSE LANDING GEAR STRUCTURE UPPER SUPPORT BEAM STA 360 HAS CORROSION FWD AND AFT SIDES. COMPLIED WITH EA F-5310-157209. MAJOR REPAIR.SDR FDEA201202030464Skin · buckledEXTERNAL SKIN STA 1720 - 1740 BETWEEN S-27L TO S-29L BUCKLING. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-01, FIG 101, DET III. ACCOMPLISHED EA F-5330-159906. MAJOR REPAIR.
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