N913FD
Service difficulty reports · 184
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 = 'N913FD' 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 = 'N913FD' 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 FDEA201704061394Skin · damagedRIGHT INBD MAIN FLAP DENTED AND DELAMINATED ON PREVIOUS REPAIR UPPER SURFACE. REPAIRED THE DAMAGED UPPER SKIN & HONEYCOMB IAW SRM 57-53-01, REPAIR 1, FIGURE 201, AND SRM 51-70-10, REPAIR 4, FIGURE 201, REV 120.SDR FDEA201704061392Skin · delaminatedLEFT INBD AFT FLAP PUNCTURED ON THE UPPER INBD SURFACE. REPAIRED IAW SRM 51-70-17, PARAGRAPH 4(B), REV 120.SDR FDEA201704061374Crease Beam · corrodedCORROSION ON CREASE BEAM BETWEEN BS 860 - 880. OUT OF ALLOWABLE LIMITS IAW SRM 53-30-13, FIGURE 101, DETAIL VIII, REV 120. REPAIRED IAW EA F-5310-T0332845.SDR FDEA201704051342Support · corrodedSUPPORT STRUCTURE UNDER WING TO BODY FAIRING 193, CORRODED UNDER ANCHOR NUT. REPAIRED THE SUPPORT STRUCTURE IAW SRM 53-40-71, FIGURE 201, AND SRM 51-70-11, FIGURE 1, DETAIL 1, REV 120.SDR FDEA201704051393Panel · damagedNR 7 LE SLAT HAS DAMAGE ON LOWER TRAILING EDGE CLOSURE PANEL, 21 INCHES FROM INBD END. REPAIRED THE PANEL IAW SRM 51-70-07.SDR FDEA201704051387Attach Fitting · missingFRAME FOOT FOUND MISSING AT BS 620 BETWEEN STRINGERS 27 AND 28L. INSTALLED THE FRAME FOOT IAW SRM 51-40-02, REV.120SDR FDEA201704051373Fitting · crackedNR 1 PYLON, STRUT TO DIAGONAL BRACE ATTACH FITTING CRACKED. REPAIRED IAW EA F-5450-T0332426.SDR FDEA201704051344Floor Support · corrodedCORROSION ON SIDE OF FWD CARGO FLOOR SUPPORT LBL 2.90 AT BS 748. FORWARD CARGO FLOOR SUPPORT REPAIRED IAW SRM 53-00-53, REPAIR 1, REV 120.SDR FDEA201704051341Angle · crackedCRACK ON ANGLE BS 1180, STRINGER 29L, UNDER WING TO BODY FAIRING 197LL. REPLACED THE ANGLE IAW SRM 51-40-02.SDR FDEA201704031267Panel · delaminatedDELAMINATION INSIDE THE VERTICAL STAB, LT SIDE PANEL AT VSS 200, 2 LOCATIONS. REPAIRED IAW EA F-5530-T0335605.SDR FDEA201704031183Floorbeam · crackedCRACK ON CABIN FLOORBEAM BS 580, LBL 48. THE FLOORBEAM REPLACED IAW SRM 51-40-02 AND DRAWING PL 657N4311.SDR FDEA201703311378Skin · tornR4 DOOR INTERNAL SKIN TORN ON AFT MID SECTION OF DOOR BETWEEN BS 1647 - 1652. REPAIRED IAW EA F-5210-T0332532.SDR FDEA201703311377Skin · crackedR4 DOOR HAD THREE STOP DRILLED CRACKS ON INTERNAL SKIN BETWEEN BS 1665 - 1679 AND STOPS 4 - 5. REPAIRED IAW EA F-5210-T0332532.SDR FDEA201703311376Skin · damagedR4 DOOR INTERNAL SKIN TORN ON FWD MID SECTION OF DOOR CRACKS BETWEEN BS 1647 - 1652 AND BEAMS 2 -3. REPAIRED IAW EA F-5210-T0332532.SDR FDEA201703301382Structure · crackedEVIDENCE OF CRACK ON THE R2 DOOR UPPER HINGE CUTOUT. REPAIRED AREA IAW SRM 52-10-02, REPAIR 1, REV 120, AND EA F-5210-T0333043.SDR FDEA201703301266Skin · crackedEVIDENCE OF CRACK ON THE L2 DOOR UPPER HINGE CUTOUT. REPAIRED IAW SRM 52-10-02, REPAIR 1, REV 120.SDR FDEA201701120160Life Raft · dislodgedRAFT IS BEGINNING TO FALL OUT OF RIGHT FORWARD ENTRY DOOR. REINSTALLED R1 DOOR ESCAPE SLIDE PER AMM 25-66-01-4. ALL OK, AIRCRAFT OK TO CONTINUE. REINSTALLED R1 DOOR ESCAPE SLIDE PER AMM 25-66-01-4. ALL OK, AIRCRAFT OK TO CONTINUE.SDR FDEA201612204509Bulb · inoperativeDURING POSTFLIGHT FOUND LH SIDE EXTERIORE EMERGENCY EXIT LIGHT INOP EMERGENCY SLIDE LIGHT BULB REPLACED PER AMM 33-51-06 REV117.6 OPS TEST SATISSDR FDEA201612084370Computer · malfunctionedDURING APPROACH, DURING LAVS PROCEDURE PRIOR TO IBM 7.0 THROTTLES WERE COMMANDED TO EPR "FULL POWER". AUTOPILOT, FMS & FLIGHT DIRECTOR HAVE OPERATED NORMAL FOR ALL OTHER OPERATIONS & APPROACHES. R & R BOTH LT & RT FMS COMPUTERS IAW AMM. TEST PASSED IAW SDR FDEA201611134012Duct · failedDURING PUSH BACK AFTER LEFT ENGINE START, LEFT DUCT LEAK APPEAED ON EICAS RAN QRH DUCT LEAK LP. FOUND BLOWN DUCT AT WELD SEAM. INSTALLED SERVICEABLE APU PNEUMATIC DUCTSDR FDEA201604201308Crank Assy · crackedON ARRIVAL FOUND L1 DOOR PART OF LOWER ESCAPE SLIDE OUT OF PLACE. ALSO PART OF GIRT BAR MECHANISM ROD AT LOWER PART IS BROKEN. RELEASED FOR SERVICE IAW MEL 52-11-01-A CATEGORY B EXPIRATION 23 APR 16. L1 DOOR SLIDE INOPERATIVE. FOUND CRANK ASSEMBLY FOR THESDR FDEA201409122602Cable · fouledLEFT AFT NOSE WHEEL STEERING CABLE FOUND FOULING ON TOP OF LT FWD PULLEY GUARD ON TOP OF NOSE GEAR STRUT. IPC 32-51-01 FIGURE 01 VIEW B SHEET 003 ITEM 320. CABLE INSPECTED & REROUTED IAW AMM 32-51-00.SDR FDEA201404250855Flex Line · crackedTAKEOFF PLUS TEN MINUTES EICAS LT HYD QTY, CREW NOTED QTY AT .60 & DECREASING AT A RATE OF APPROX .10 MINUTE. 5 - 6 MINUTES LATER LT HYD QTY WAS 0.00. EICAS LT HYD SYS PRESS FOLLOWED. LT HYD PUMP ELEC & ENG SHUTOFF AS DIRECTED BY QRH. HYD QTY WAS NEAR 0 SDR FDEA201312162996Slide · faultyL1 DOOR SLIDE PARTIALLY DEPLOYED ON DOOR OPENING. DOOR FOUND IN ARMED POSITION, DOOR ASSIST BOTTLE FIRED. SLIDE REMOVED FROM ACFT TO OPERATE IAW MEL 52-11-01-A. L1 DOOR SLIDE INOPERATIVE. L1 DOOR SLIDE EMERGENCY RESERVOIR REPLACED IAW AMM 52-11-30-004-037SDR FDEA201305060921Lamp · inoperativeR1 DOOR SLIDE ARM LIGHT DOES NOT ILLUMINATE WHEN DOOR IS ARMED,COCKPIT INDICATIONS SHOW DOOR ARMED. REPLACED LAMP IAW SMP, CYCLED DOOR SLIDE ARM LEVER NUMEROUS TIMES AND LIGHT OP'S NORMAL. A/C OK FOR SERVICE.SDR FDEA201304030721Tee Fitting · crackedR1 DOOR INTERIOR TEE IS CRACKED BS 353, WL 250. REPAIRED IAW EA F-5210-154145SDR FDEA201303310693Panel · crackedNR 2 SLAT HAS A CRACKED COVE PANEL AT OTBD MAIN TRACK ATTACH AREA OSS 677 TO OSS 705. REMOVED DAMAGED COVE SKIN ON LH WING #2 SLAT AT OB MAIN TRACK ATTACH COVE AREA, FABRICATED NEW, AND INSTALLED IAW BOEING DWG 114N4076 REV C & B757 SRM 51-40-02SDR FDEA201303310694Panel · crackedNR 2 SLAT HAS A CRACKED COVE PANEL AT INBD MAIN TRACK ATTACH AREA OSS 605 TO OSS 617. REMOVED DAMAGED PANEL, FABRICATED NEW, AND INSTALLED IAW DWG 114N4076 REV C & SRM 51-40-02.SDR FDEA201212114279Cover · unsecureRAFT COVER ON R1 IS NOT SECURED PROPERLY. SECURED SLIDE RAFT COVER AT R1 DOOR IAW 25-66-01-4 AMM. CHECKS GOOD. ACFT OK FOR SERVICE. FINAL CLOSED.SDR FDEA201210053554Girt Bar · dirtyLT CREW ENTRY DOOR VERY DIFFICULT TO OPEN. CHECKED DOOR IAW MM 52-11-00-2, FOUND L-1 DOOR LT SIDE GIRT BAR AND GIRT BAR FLOOR BRACKET NOT DISENGAGING COMPLETLY WHEN DISARMING DOOR CAUSING DOOR TO BE DIFFICULT TO UNLATCH. CLEANED LATCH AND MECHANISM OF GRISDR FDEA201110124447Latch · failedCAPT'S EMERGENCY ESCAPE ROPE DOOR WILL NOT CLOSE. REPLACED LATCH IN REF TO SRM 51-40-02-0G-0. REINSTALLED CAPTAINS ESCAPE ROPE AND CLOSED DOOR IAW MM 25-61-00-4-0. ACFT OK FOR SERVICE.SDR FDEA201107252943Battery Pack · failedR1 DOOR EMERGENCY EXIT LIGHTS INOP DURING A TEST. R & R R1 EMERGENCY EXIT LIGHT BATTERY PACK IAW MM 33-51-07-2. OPS CHECKED NORMAL.SDR FDEA201104141499Skin · dented2 DENTS STA 1608, STR 13L. REPAIRED DAMAGED AREA BY COMPLYING WITH EA F-5330-150144 FUSELAGE-FUSELAGE SKIN AT STATION 1608/STRINGER 13L-DENTSSDR FDEA201104141490Skin · dentedDENT STA 1716 AT STR 14R LAP SEAM. CUT OUT DAMAGED AREA IN UPPER SKIN 13' X 7 3/4" X 3" AND LOWER SKIN 5 3/4" X 3", AND FABRICATED AND INSTALLED FILLER, STRUCTURAL FILLER, DOUBLER, AND TRIPLER IAW E.A. F-5330-123590SDR FDEA201011064268Sensor · failedLT ENTRY DOOR SLIDE INTERMITT SLIDE INDICATOR. LIGHT FLASHED ON AND OFF WHEN F/O WENT TO DISARM SLIDE AFTER FLIGHT. R & R AFT GIRTH BAR PROX SWITCH S10215 IAW AMM 25-66-11-2. OPS CHECK GOOD. (CLOSED)SDR FDEA200910223647Frame Splice · damagedMAIN CABIN DECK STA 1280, STR 12 & 13, LT HAS A FRAME REPAIR SPLICE DAMAGE. REMOVED REPAIR ANGLES IAW SRM 51-40-02, RECIEVED NEW FROM FAB SHOP 2EA REPAIR ANGLES, MAE TRAV T9/805465, INSTALLED NEW REPAIR PARTS STA 1280, STR 12 & 13, LT IAW SRM 53-00-07, FIGSDR FDEA200910223646Frame Splice · damagedMAIN CABIN DECK STA 1280, STR 12 & STR 13, RT HAS FRAME REPAIR SPLICE DAMAGE. REMOVED REPAIR ANGLES, FABRICATED NEW SPLICE REPAIR ANGLES, MAE TRAV T9/805464, INSTALLED REPAIR PARTS AT STA 1280, STR 12 & 13 RT, IAW SRM 53-00-07, FIG 201, REPAIR 2. MAJOR REPAISDR FDEA200910133554Skin · corrodedNR 1 PYLON, INBD AFT SKIN ASSY HAS CORROSION. REMOVED CORROSION, REMOVED SKIN IAW SRM 54-50-01. FABRICATED NEW SKIN ON MAE TRAV NR T9/803805. INSTALLED NEW SKIN PANEL ASSY INBD AFT IAW EA NR F-5450-131114. MAJOR REPAIR.SDR FDEA200910063486Skin · delaminatedDELAMINATION ON SLAT NR 6, TRAILING WEDGE, ABOUT 30" FROM INBD EDGE. ACCOMPLISHED REPAIR OF RT WING, NR 6 L/E SLAT, T/E WEDGE, ABOUT 30" FROM INBD END IAW EA F5750-133518, SRM 51-70-10, REPAIR NR 4, AND SRM 57-43-02. THIS REPAIR IS CLASSIFIED AS A CAT "A" MAJOSDR FDEA200909303446Skin · dentedPROTRUDING DENT BETWEEN STA 324- 333.45, STR 22- 23 LT SIDE FUSLAGE. AFTER EVAL, DENT OUT OF LIMITS IAW SRM 53-00-01, FIG 101, DET III, CUT OUT DAMAGE AREA, FABRICATED REPAIR DOUBLER AND FILLER, INSTALLED REPAIR IAW SRM 51-40-02, AND SRM 53-00-01, FIG 201, SDR FDEA200909233372Floorbeam · corrodedFWD CABIN, FLOORBEAM (BULKHEAD) AT BS 324, RBL 26-RBL 60, UPPER SURFACE HAS SEVERAL AREAS OF CORROSION. REMOVED CORROSION IAW SRM 51-10-02. ORIGINAL MATERIAL THICKNESS .125, AFTER REWORK .106 INCH, REMOVED .019 INCH; L=2 INCHES, W=2 INCHES, D=.019 INCH, FOUNSDR FDEA200909223365Skin · damaged3 EA LIGHTENING STRIKES FOUND DURING SCRIBELINE LAP SEEM INSP LOCATED AT BS 1440.125 S-4R AND BS 1449.500 S-4R IN THE LAP SEAM. EACH MARKED WITH DOT. DOT 137-001 ACCOMPLISHED EA F-5330-131525. THIS IS A CAT B REPAIR WITH INSPECTIONS EVERY 3000 FC'S INCLUDINSDR FDEA200909163310Panel · debondedLT WING UPPER INBD FIXED PANEL EXT- SKIN AT RSTA 177.5, PANEL MOUNTING HOLES ELONGATED SKIN BULGING / DISBONDED. ACCOMPLISHED EA F- 5730-131110, THIS REPAIR HAS RECEIVED FIRST STAGE APPROVAL, THE DTA WILL BE TRACKED VIA ENMDS, 24 MONTHS FROM FAA FORM 8100-9SDR FDEA200909123293Skin · crackedNR 1 PYLON OTBD AFT 311N5046-31 SKIN ASSY HAS 2 EA FASTENER HOLES WITH VISIBLE CRACKS AT APROX PPS 153.90 NDT HFEC INSPECTED VERIFIED CRACKS IAW NTM, 51-00-19 PART 6, (CRACK LENGTHS ARE 1=0.250 INCH, 2= .0200 INCH, 3= 0.198 INCH, STOP DRILLED CRACKS IAW EA F-5SDR FDEA200909123292Skin · corrodedRT NAC- FWD INBD SKIN INNER WALL CORRODED, JUST AFT OF 443 GL ACCESS PANEL CUT-OUT. REMOVED CORROSION IAW SRM 54-50-01 FIG 101 L=1.0 INCH, W=1.0 INCH, D=0.035 INCH, ORIGINAL MAT. 0.90 INCH, MAT REMAINING 0.055 INCH FOUND TO BE OUT OF LIMITS IAW SRM 54-50-01 FISDR FDEA200909123291Skin · corrodedLT PYLON EXT LWR OTBD SKIN JUST BELOW MID SPAR FUSE PIN (APROX PP-185 TO PPS-196 ) HAS CORROSION. REMOVED CORROSION IAW SRM 54-50-01, DETAIL 1 AND FIG 101. ORIGINAL MAT 0.090 INCH, REMAINING MAT. 0.074 INCH, L=12.0 INCH, W=1.75 INCH, D=0.016 INCH FOUND TO BESDR FDEA200909123290Skin · corrodedNR 1 PYLON OTBD AFT 311N5046-31 SKIN ASSY HAS CORROSION ON INTERIOR SURFACE BETWEEN FWD ACCESS DOOR OPENING AND PRECOOLER OPENING. REMOVED CORROSION FROM INTERIOR SURFACE IAW SRM 54-50-01 ORIGINAL MATERIAL 0.90 INCH, MATERIAL LOSS 0.013", MAT REMAINING 0.077 SDR FDEA200909093278Skin · misrepairedPREVIOUSLY INSTALLED REPAIR IDENTIFIED AT BS 1610, S-17L/18L, HAS UNDERSIZED FASTENERS. REMOVED EXISTING DOUBLER IAW SRM 51-40-02. CUT OUT DAMAGED AREA IAW SRM 53-00-01. REPAIR 3 FIG 201. INSPECTED CUT OUT AND OPEN HOLES FOR CRACKS, NO CRACKS FOUND IAW NSDR FDEA200909013210Pressure Panel · corrodedON PRESSURE DECK UPPER SURFACE FWD OF BS 1040, BELOW CREASE BEAM STR- 18L. ACCOMPLISHED EA NR F-5710-131109, WING CTR SECTION - UPPER SKIN CORROSION REPAIR, LBL 62, STA 1040, AND REAR SPAR , FAA FOR 8100-9, DATED 08/21/2009 ATTACHED.SDR FDEA200909013209Crease Beam · misalignedWHILE PERFORMING PTF SECTION 46 RT CREASE BEAM MOD, PRODUCTION FOUND A MISMATCH INBD TO OUTBD BETWEEN THE CREASE BEAM INNER CHORD AT THE PRODUCTION SPLICE AT APPROX STA 1628, RBL 63. A REPAIR WAS ACCOMPLISHED AT STA 1590-1628, RBL 63, CREASE BEAM INNER CHORD
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