N733FD
Service difficulty reports · 203
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 = 'N733FD' 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 = 'N733FD' 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 FDEA201410183297Rib · corrodedCOMPLIED WITH EA 6-5710-T0311733 PT 1, PT 2 & PT 3 WINGS BASIC WING STRUCTURE RT RIB 5 REPLACEMENT. MAJOR REPAIR.SDR FDEA201409302868Lug · corrodedLEFT RIB 5 FWD LUG HAS CORROSION IN THE BORE & FACES. COMPLIED WITH EA 6-5710-T0311839 P1 WINGS BASIC WING STRUCTURE LT RIB 5 FWD LUG CORROSION.SDR FDEA201408082119Door Frame · dentedFORWARD CARGO DOOR CUT OUT FWD FUSELAGE FRAME FOUND A DENT AT STRINGER 40R - 41R. REPAIRED THE DENT PER EA 6-5310-T0310229 TITLE:FUSELAGE-MAINFRAME-ONE DENT ON FRAME FR20A WEB AT STRINGER 40R MAJOR REPAIR IAW GMM 6-2-100SDR FDEA201407251964Frame · crackedFRAME 47 FOUND TO HAVE A CRACK SIGNAL DURING NDT CHECK. REPAIRED IAW EA 6-5710-T0310210. MAJOR REPAIR IAW GMM 6-2-100.SDR FDEA201407251961Frame · crackedFRAME 47 FOUND TO HAVE A CRACK SIGNAL DURING NDT CHECK. REPAIRED IAW EA 6-5710-T0310210. MAJOR REPAIR IAW GMM 6-2-100.SDR FDEA201407251960Frame · crackedFRAME 40 FOUND TO HAVE A CRACK SIGNAL DURING NDT CHECK. REPAIRED THE FRAME IAW EA 6-5710-T0310489A. MAJOR REPAIR IAW GMM 6-2-100.SDR FDEA201407251967Frame · crackedFRAME 47 FOUND TO HAVE A CRACK SIGNAL DURING NDT CHECK. REPAIRED IAW EA 6-5710-T0310210. MAJOR REPAIR IAW GMM 6-2-100.SDR FDEA201407251965Frame · crackedFRAME 47 FOUND TO HAVE A CRACK SIGNAL DURING NDT CHECK. REPAIRED IAW EA 6-5710-T0310210. MAJOR REPAIR IAW GMM 6-2-100.SDR FDEA201407251963Frame · crackedFRAME 47 FOUND TO HAVE A CRACK SIGNAL DURING NDT CHECK. REPAIRED IAW EA 6-5710-T0310210. MAJOR REPAIR IAW GMM 6-2-100.SDR FDEA201407251959Frame · crackedFRAME 40 FOUND TO HAVE A CRACK SIGNAL DURING NDT CHECK. REPAIRED THE FRAME IAW EA 6-5710-T0310489. MAJOR REPAIR IAW GMM 6-2-100.SDR FDEA201407251958Frame · crackedFRAME 40 TO CTR WING JOINT AT UPPER SKIN LEVEL TENSION BOLT JUNCTION FOUND CRACK SIGNAL BY NDT CHECK. REPAIRED FRAME IAW EA 6-5710-T0310489. MAJOR REPAIR IAW GMM 6-2-100.SDR FDEA201407251957Frame · crackedFRAME 40 TO CTR WING JOINT AT UPPER SKIN LEVEL TENSION BOLT JUNCTION FOUND CRACK SIGNAL BY NDT CHECK. REPAIRED FRAME IAW EA 6-5710-T0310489. MAJOR REPAIR IAW GMM 6-2-100.SDR FDEA201407251956Frame · crackedFRAME 40 TO CTR WING JOINT AT UPPER SKIN LEVEL TENSION BOLT JUNCTION FOUND CRACK SIGNAL BY NDT CHECK. REPAIRED FRAME IAW EA 6-5710-T0310489.SDR FDEA201311022669Turbine · damagedENROUTE, NR 2 ENGINE STARTED A SEVERE VIBRATION, COMPLIED WITH JRH. PRECAUTIONARY SHUTDOWN. DIVERTED. REMOVED AND REPLACED NR 2 ENGINE DUE TO TURBINE DAMAGE IAW 64T0712-2. LEAK AND OPS CHECKED NORMAL. IAW JRH RUN COMPLETED.SDR FDEA201310172539Selector · leakingENROUTE, GREEN SYS FLUID IN RESEVOIR DECREASED TO RED DOT ECAM PROCEDURES. PUMPS TURNED OFF AND NR 6 SPOILER. GRAVITY EXTENDED GEAR. R & R THE GREEN SYS MANIFOLD SERVO CONTROL MODULE IN REF TO AMM 29-11-34-04 AND R & R SERVO CONTROL SELECTOR VALVE IAW AMM 2SDR FDEA201305161010Wire Harness · chafedAFTER TAKEOFF AT APPROX 800 FT AGL, GENERATOR 2 FAULTED AND AC BUSS 2 FAILED. ALL RELATED SYS FAILED. ABLE TO RESET GENERATOR 2 AND RECOVERED AC BUSS 2. ABLE TO RESET ALL RELATED SYSTEMS, INSPECTED E&E COMPARTMENT FOR EVIDENCE OF WATER, CHECKED GCU'S FOR SDR FDEA201203281158Pressure Switch · failedIN-FLIGHT ENG NR 1 SHUTDOWN DUE TO ENG OIL CLOG LIGHT WOULD NOT GO OUT. REF FIM 79-00-20, FIG 109. PERFORMED INSPECTION CHECK OF MASTER CHIP DETECTOR IAW AMM CH 79-22-03-06-0. CHIP DETECTOR WITHIN PARTICLE LIMITS. R & R SCAVENGE OIL FILTER ELEMENT IAW AMMSDR FDEA201202220641Intercostal · crackedFWD CARGO BAY FR 38.1 LT, S44L, 8" BELOW ROLLER TRACK 3L, INTERCOSTAL WEB HAS CRACK AT LOWER FWD ATTACH POINT 1.5" LONG. R & R FWD CARGO COMP FR 38.1 LT INTERCOSTAL BELOW ROLLER TRACK 3 REF TO SRM 51-40-21. PERFORMED OPS CHECK, OPS CHECK SATISFACTORY REF TO SDR FDEA201202190617Stiffener · gougedNR 1 PYLON PANEL 413 CL HAS .50" GOUGE AT MILLED STIFFENER. COMPLIED WITH EA 6-5480-156100 NACELLES/ PYLONS INSTALLED REPAIR DOUBLER IAW SRM 54-52-51, FIG 202, SHEET 1, PGS 209-210.SDR FDEA201202190616Stiffener · crackedNR 2 ENGINE ANTI-ICE NOSE COWL DUCT TIE ROD SUPPORT BRACKET HAS 2 EA ELONGATED HOLES. COMPLIED WITH EA 6-5450-156097 NACELLES/PYLONS. REPAIRED NR 2 CANTILEVER BEAM AT RIB A7. R & R STIFFENER AT RIB A7 IAW SRM 51-72-10SDR FDEA201202140572Door Frame · crackedAFT CARGO DOOR CUT OUT UPPER SILL PROFILE PANEL FWD SIDE CRACKED APP. L=2" WORKED WITH WORK CARD 51003551. REMOVED AND REINSTALLED AFT CARGO DOOR ACTUATOR TO FOM IAW AMM 52-32-11-04-01, OPS TEST ON DOOR GOOD IAW AMM 52-32-11-05-01 AND AMM 52-73-00-05-01. RSDR FDEA201202080517Panel · corrodedRT PYLON NOSE COWL FAIRING PANEL 421AL BOTTOM SURFACE CORROSION AROUND SCREW HOLE APP. L=2",W=1.5". REMOVED CORROSION ON ARCH PANEL 421AL NR 2 ENGINE PYLON IAW SRM 51-74-10, PG. 205 PAR.3, CHECKED LIMITS FOUND TO BE BEYOND LIMITS IAW SRM 54-50-00, PG 111 PSDR FDEA201202020437Floorboard · damagedFLOORBOARD 241 DF HAS APPROX. 1.5 OF COMPOSITE & BOTTOM PLY MISSING ON RT SIDE APPROXIMATEY AFT OF FORWARD EDGE. FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 25-005, REV J.SDR FDEA201202020436Floorboard · corrodedBULK CARGO FLOORBOARD 161HF HAS 30"SQ IN OF CORROSION ON METALLIC OVERLAY FABRICATED REPLACEMENT FLOORBOARD 161HF IAW DWG, SRZ 25-011 D.SDR FDEA201202020435Floorboard · crackedBULK CARGO FLOORBOARD 161GF HAS 6 EA CRACKS FROM .2500" TO 2' LONG IN METALLIC OVERLAY PENTENING INTO UNDERLINE COMPOSITE FABRICATED REPLACEMENT FLOORBOARD 161 GF IAW DWG SRZ 25-005, REV J & DWG SRZ 25-011, REV D.SDR FDEA201202010418Floorboard · crackedFORWARD CARGO FLOORBOARD 131 QF HAS 5 EACH CRACKS 1" TO 4". FABRICATED REPLACEMENT FLOORBOARD 131 QF IAW DWG SRZ 25-005, REV J.SDR FDEA201201310400Floorboard · crackedFLOORBOARD 242 EK BOTTOM PLY & HONEYCOMB IS CRACKED ACROSS WIDTH OF THE FLOORBOARD APPROX 20" AFT OF FWD EDGE. FABRICATED FLOORBOARD 242 EK IAW DWG NR SRZ 25-005, REV J.SDR FDEA201201310399Floorboard · delaminatedAFT CARGO FLOORBOARD 151 DF HAS 12' SQ IN OF EDGE DELAMINATION WITH EDGE DAMAGE. FABRICATED FLOORBOARD 151 DF IAW DWG SRZ 25-005, REV J.SDR FDEA201201310398Floorboard · crackedAFT CARGO FLOORBOARD 151 GF HAS 2 CRACKS, AT EDGE .5 AND 1 IN MIDDLE OF PANEL FROM SIDE TO SIDE. FABRICATED REPLACEMENT FLOORBOARD 151 GF IAW DWG SRZ 25-005, REV J.SDR FDEA201201310397Floorboard · delaminatedFORWARD CARGO FLOORBOARD 132 ZF HAS 40" SQ IN OF SURFACE DELAMINATION. FABRICATED REPLACEMENT FLOORBOARD 132 ZF IAW DWG SRZ 25-005, REV J.SDR FDEA201201310396Floorboard · damagedFORWARD CARGO FLOORBOARD 132 RF HAS 30" SQ IN EDGE DAMAGE FABRICATED REPLACEMENT FLOORBOARD 132 RF IAW DWG SRZ 25-005 REV JSDR FDEA201201310395Floorboard · crackedAFT CARGO PIT FLOORBOARD 151 BF HAS 4" SQ IN EDGE DAMAGE WITH 2 CRACKS 1" LONG FABRICATED REPLACEMENT FLOORBOARD 151 BF IAW DWG SRZ 25-005, REV J.SDR FDEA201201300383Floorboard · damagedFWD CARGO COMPARTMENT FLOORBOARD 131 HG HAS IMPACT DAMAGE MEASURING 4" LONG AT LWR EDGE. FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 25-005, REV J.SDR FDEA201201300382Floorboard · damagedFLOORBOARD 241 RJ FWD SECTION IS COMPLETELY BROKEN OFF. FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 25-005, REV J.SDR FDEA201201270360Crossbeam · corrodedAFT CARGO COMPT FR58 RT SIDE 3" FROM CENTERLINE, UNDERSIDE INBD OF ROLLER TRACK 1R, 1 SQ IN OF CORROSION. PERFORMED REPAIR IAW SRM 53-10-15 PG 237-242 FIG 207.SDR FDEA201110104416Rib · corroded1" X 2" AREA OF CORROSION FOUND ON LT LOWER SKIN RIB 5 DOUBLER AROUND FASTENER HOLE. REPAIRED IAW EA 6-5710-145618, PT 1.SDR FDEA201107042565Pitot Line · obstructedDURING T/O ROLL BOTH PFDS DID NOT DISPLAY ANY AIRSPEED INDICATIONS. BOTH STBY AIRSPEED INDICATORS WORKED. REJECT AT 100KTS. PREFORMED PITOT LEAK TEST ON BOTH CAPT'S AND F/O'S AIRSPEED. NOTICED WHEN AIRSPEED WAS ON THE WAY DOWN THE AIRSPEED INDCATIORS WERSDR FDEA201009263713Controller · malfunctionedUPON LOWERING FLAPS TO 20 DEGREES FOR LANDING,GOT FLAPS STUCK ECAM.WENT AROUND AFTER CYCLING HANDLE GAVE NO HELP. ECAM MESSAGE THEN CHANGED TO FLAP SYSTEM 1 FAULT/FLAPS SLOW.REMAINDER OF CONFIGURATION FOR LANDING WAS NORMAL. COMPLETED TSM 27-50-01 ITEMS, NO SDR FDEA201007212635Smoke Detector · failedAVIONICS SMOKE INDICATION. PIGGY-BACKED KNOWN GOOD DETECTOR TO 11WA AND CKS GOOD. REMOVED AND REPLACED 11WA IAW MM.SDR FDEA201002100379Wire · burnedNR 1 GEN FAULT AS TAKEOFF POWER APPLIED. WOULD NOT RESET. ABORTED AT 80 PERCENT POWER AT 30 KNOTS, RECONFIGURED WITH APU & DEPARTED. RELEASED FOR SERVICE IAW MEL: 24-11-01-B. APU GEN MUST BE USED TO POWER AFFECTED BUSS THROUGHOUT FLIGHT. MAX ALT FL 350. VERSDR FDEA200909013206Skin · corrodedFOLLOW UP INSP IAW EA 6-5710-110701A PT 2 REVEALED ADDITIONAL CORROSION IN FASTENER HOLES. COMPLIED WITH EA 6-5710-110701B PT 3 BY OVERSIZING HOLES AND INSTALLING OVERSIZED FASTENERS IAW RAS/BAE/ 017/2009 ISSUED AND REMOVING CORROSION.SDR FDEA200908293121Skin · chafedRT INBD FLAP UPPER SKIN HAS 2 EA AREAS CHAFED, MAX DEPTH 0.016 INCHES, DAMAGE FOUND TO BE OUT OF LIMITS IAW SRM 57-50-00,FIG 101. CUT OUT DAMAGED AREA ON RT INBD FLAP UPPER SKIN AND INSTALLED FLAP SKIN/STRINGER REPAIR BETWEEN FLAP RIBS NR 11 AND NR 12, STSDR FDEA200908283119Skin · dentedRT WING CTR FLAP LOWER SKIN HAS DENT, MEASURES 3.250 IN X 2.250 IN X 0.680 IN DEEP AND HAS RIVETS WITHIN THE DENT. DENT IS OUT OF LIMITS IAW SRM 57-50-020, PG BLOCK 101 CUT OUT DAMGED AREA AND INSTALLED FLAP SKIN PATCH REPAIR ON RT WING CTR FLAP LWR SKIN BETSDR FDEA200908223069Seat Track · damagedMDCC SEAT TRACK 2R 2 IN. FWD OF FR 54.3 HAS 1 EA DAMAGED SCALLOP. REMOVED DAMAGED SEAT TRACK AT 2R FWD OF FR 54.3. INSTALLED REPAIR SECTION SEAT TRACK AND 2 EA REPAIR SPLICES IAW SRM 53-10-16.SDR 08FDEA00440Sequence Valve · failedAFTER TAKEOFF FROM KIAD, THE RIGHT MAIN LANDING GEAR FAILED TO RETRACT AND REMAINED FULLY DOWN AND LOCKED ON BOTH FORWARD AND OVERHEAD PANEL INDICATIONS. FOLLOWED ECAM AND QRH PROCEDURES, GOT DOWN AND LOCKED INDICATIONS ON ALL 3 GEAR. THEN RETURNED TO LAND SDR 07FDEA05059Idg · underservicedON TAKEOFF ROLL AT IND, ABOUT 50 KTS NR 2 GENERATOR FAULTED, ACCOMPLISHED RTO CK LIST, AND RESET GEN, AFTER RESET WORKED OK. FOUND IDG UNDER SERVICED, SERVICED PER AB MM 24-11-00-3-02, RAN ENG OPS CK OK. FOUND IDG UNDER SERVICED, SERVICED PER AB MM 24-11-00-SDR 07FDEA04299Skin · crackedFOUND AT LT INNER FLAP LOWER SKIN CRACKED (4MM) AND HOLES DAMAGED REPAIR PERFORMED BY REMOVAL OF CRACKS AND OVERSIZING THE DAMAGED HOLES IAW EA 6-5752-112505 AND RAS/FOK/024/2007 ISS A.SDR 07FDEA04298Fitting · crackedCRACK FINDINGS AT LT CENTER WING C 47 VERTICAL FLANGE ANGLE FITTING HOLE NR H (A=33MM,B=31MM) AND NR I (A=12MM,B=10MM) REPAIR PERFORMED BY OVERSIZING HOLE NR H, I UNTIL CRACK AND CUT THE EXTERNAL FITTING REMOVAL IAW EA 6-5710-112497 AND RAS/053592/015/2007.SDR 07FDEA04297Fitting · crackedCRACK FINDINGS AT RT CENTER WING C 47 VERTICAL FLANGE ANGLE FITTING HOLE NR H (A=55MM,B=30MM) AND NR N (A=32MM,B=31MM) AND NR 39 WITH BUSH REPAIR AND INCORRECT FASTENER INSTALLED. REPAIR PERFORMED BY OVERSIZING HOLE NR H, N UNTIL CRACK REMOVAL AND INSTALLING SDR 07FDEA04274Deflector · damagedFOUND DAMAGED EDGE BAND OF DEFLECTOR DOOR 572CB AT LT WING. BONDING REPAIR PERFORMED IAW SRM 51-77-12, APPROVED BY EA 6-5755-112454 AND RAS/BAE/1005223/2007 ISSUE A.
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