N792FD
Service difficulty reports · 62
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 = 'N792FD' 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 = 'N792FD' 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 FDEA202610151597Lamp · inoperativeL1 DOOR EXTERIOR EMERGENCY LIGHT INOP. AMM: 33-51-06-2-1 RELAMPED L1 DOOR EXTERIOR SLIDE LIGHT, OP'S CHECKS GOODSDR FDEA202610041472Lamp · failedL1 DOOR EXTERNAL EMERGENCY LIGHT DOES NOT ILLUMINATE DURING TEST. AMM: 33-51-06-2-1 CLEANED SOCKET CONTACTS AND RELAMPED, OPS CKS GOOD, OK FOR SERVICE.SDR FDEA202504280684Fuel Control · faultedFOLLOWING RIGHT ENGINE START, FLIGHT CREW NOTICED YELLOW FLASH ON RIGHT SIDE OF AIRCRAFT AS WELL AS LOSS OF N1 INDICATION ALONG WITH SMELL OF JET FUEL. NO FIRE WARNING WAS PRESENT ON EICAS. ENGINE WAS KEPT RUNNING FOR A SHORT TIME, BEFORE SHUTTING DOWN BSDR FDEA202412181814Light · brokenAFT COCKPIT DOME LIGHT FIXTURE BROKEN WITH BOTH MAIN & EMERGENCY LAMPS INOP. VERIFIED NO POWER ON DOME LIGHT MODULE ON BOTH WIRES W0200-0006 & W0200-0007. FLT DECK DOME LIGHTS CAN NOT BE DIMMED, SUSPECT BAD DOME LIGHTS DIMMER TRANSFORMER. DISCOVERED CB P34B SDR FDEA202408311211Door · no discrepancyUNABLE TO ARM L1 DOOR. OPS CHECK L1 DOOR ARMED AND DISARMED, NORMAL. NO DEFECTS NOTED AT THIS TIME. OPS CHECK WAS GOOD. A/C OK FOR SERVICE. OPS CHECK L1 DOOR ARMED AND DISARMED, NORMAL. NO DEFECTS NOTED AT THIS TIME. OPS CHECK WAS GOOD. A/C OK FOR SSDR FDEA202408311210Girt Bar · detachedWHEN OPENING THE L1 DOOR THE GIRT BAR SLIDER FELL OFF REINSTALLED GIRT BAR SLIDER PER AMM 25-66-10-02 SLIDE OPS CHECKS GOOD, NO DEFECTS NOTED. REINSTALLED GIRT BAR SLIDER PER AMM 25-66-10-02 SLIDE OPS CHECKS GOOD, NO DEFECTS NOTEDSDR FDEA202408021079Seat Track · corrodedMAIN CABIN SEAT TRACK LBL 45.50 STA 1185 BOTH FLANGES CORRODED REMOVED CORROSION ON MAIN CABIN SEAT TRACK LBL 45.50 STA 1185 BOTH FLANGES. AFTER EVALUATION FOUND TO BE OUT OF LIMIT IAW B757 SRM 53-00-52-1A FIG 101 NOTES E DETAIL VII SHEET 1 AND 4. FABRICASDR FDEA202407311074Shear Tie · corrodedAFT CARGO COMPARTMENT STA 1440 BTW STR 30 AND 29R SHEAR TIE CORRODED EVALUATED CORROSION ON SHEAR TIE AT AFT CARGO STA 1440 BETWEEN STR S-30 - 29R FOUND TO BE OUT OF LIMIT IAW B757 SRM 53-00-07-1A FIG 101 DETAIL II SHEET 3. FABRICATED NEW SHEAR TIE BDWG #SDR FDEA202407311073Seat Track · corrodedSEAT TRACK CORROSION NOTED AT STA 1320 RBL 24.75 REMOVED CORROSIOM AT SEAT TRACK FLANGE BS 1320 RBL 24.75. EVALUATED AREA ORIGINAL MAT -.070 MAT LOSS - .040 REMAINING MAT .030 FOUND TO BE OUT OF LIMITS IAW B757 SRM 53-00- 52-1A DETAIL VII FIG 101 SHEET 4. SDR FDEA202407311072Seat Track · corrodedMAIN CABIN SEAT TRACK FLANGE AT BS 1320.0 RBL 45.50 HAS AREA WITH CORROSION. REMOVED CORROSION AT MAIN CABIN SEAT TRACK FLANG AT BS 1320.0 RBL 45.5. EVALUATED SEAT TRACK FLANGE FOUND TO BE OUT OF LIMIT IAW B757 SRM 53-00-52-1A FIG 101 DETAIL I SHEET 2. FABSDR FDEA202407301069Seat Track · corrodedMAIN CABIN SEAT TRACK LBL 58.22 STA 1185 SPOT WITH CORROSION EVALUATED CORROSION ATMAIN CABIN SEAT TRACK LBL 58.22 STA 1185 NO ALLOWABLE DAMAGE ALLOWED ON SEAT TRACK IAW B757 SRM 53-00-52-1A FIG 101 SHEET 1. FABRICATED NEW SEAT TRACK IAW BDWG# 657N3321 RESDR FDEA202301120088Warning Bell · false activationFIRE BELL SOUNDED CONTINUOUSLY IN FLIGHT FROM V1 TO LANDING. WOULD NOT CANCEL WITH ALARM OFF BUTTON OR EITHER MASTER WARNING. CYCLED POWER, PERFORMED OPS TEST. OPS CHECKED NORMAL. NO HISTORY NOTED.SDR FDEA202206301629Door · openACCESS DOOR OPENED AFTER TAKEOFF. AIR TURN BACK. INSPECTED DOOR NO DAMAGE FOUND. C/W OPS CHECK OF DOOR AND NO ISSUES WERE FOUND.REF AMM 52-48-00-0. AC OK FOR SERVICE.SDR FDEA202205221276Attach Angle · crackedRMLG W/W APPROX STA 1155,AFT O/B SECTION,PANEL ATTACH ANGLE JUST BELOW THE OW SLIDE AREA IS CRACKED. REMOVED AND REPLACED PER FEDEX EA # F-5350-T0368476-P1SDR FDEA202205221275Skin · dentedEXTERIOR FUSELAGE SKIN HAS A PROTRUDING DENT AT APPROX STA 602 APPROX 1.5IN BELOW THE LAP SEAM AT S26L REPAIRED PER FEDEX EA # F-5330-T0368480SDR FDEA202205221274Skin · dentedEXTERIOR FUSELAGE SKIN HAS A PROTRUDING DENT AT APPROX STA 642 APPROX 2IN BELOW THE LAP SEAM AT S26L REPAIRED PER FEDEX EA # F-5330-T0368479SDR FDEA202205221272Panel · crackedR/W #8 SLAT I/B MAIN TRACK LOWER AERODYNAMIC PANEL HAS 2EA CRACKS ON THE I/B AND O/B SIDES OF PANEL REMOVED AND REPLACED PANEL PER BAC DWG # 114N4148 REV ASDR FDEA202205181254Skin · wornDURING AGING AIRCRAFT INSPECTION, FOUND EXISTING COMPOSITE REPAIR WITH WORN MARK, LOCATED ON RIGHT WING INBOARD MAIN FLAP OUTBOARD CORNER, UPPER SURFACE, MF STA 300.38 REPAIRED RIGHT WING INBOARD MAIN FLAP UPPER SKIN PANEL IAW FEDEX E. A. # F-5750-T0368450 TSDR FDEA202205181253Floorbeam · corrodedAFT CABIN FLOOR SUPPORT CORRODED AT FASTENER HOLES BS 1680 RBL10 TO LBL3 REMOVED DAMAGE FROM FLOOR BEAM UPPER - FORWARD FLANGE AND REPAIRED IAW B757-2 SRM 53-60-51-2R FIG 201 - REPAIR#3, RESTORED AREA PER SRM 51-20-01SDR FDEA202205181252Support Bracket · cracked#2 PYLON ,HYDRAULIC BAY,O/B SIDE,LOWER FWD CORNER,SUPPORT BRACKET IS CRACKED REMOVED AND REPLACED PER BAC DWG # 313N3052 REV BSDR FDEA202205151210Skin · wornR/H WING #8 SLAT T/E WEDGE LOWER SURFACE IS WORN IN LINE WITH THE INBD MAIN TRACK. REPAIRED R/H WING #8 SLAT T/E WEDGE LOWER SURFACE WORN IN LINE WITH THE INBOARD MAIN TRACK IAW B757 SRM 57-43-02-2R-1 FIG 201 SHEET 4 AND 51-70-10-2R REPAIR 4.SDR FDEA202205131203Web · damagedMAIN CARGO DOOR - AFT PRESSURE DOOR - CLOSE OUT WEB IS DAMAGED REMOVED, FABRICATED AND INSTALLED WEB IAW B757 SRM 51-40-02-0G ANS IAW BOEING DWG 65-49309 REV D. APPLIED ALODINE, PRIMER AND CIC IAW B757 SRM 51-20-01-0GSDR FDEA202205131202Web · damagedMAIN CARGO DOOR - FWD PRESSURE DOOR - CLOSE OUT WEB IS DAMAGED REMOVED, FABRICATED AND INSTALLED WEB IAW B757 SRM 51-40-02-0G IAW BOEING DWG # 65- 49309 REV D APPLIED ALODINE, PRIMER AND CIC IAW B757 SRM 51-20-01-0GSDR FDEA202205111179Skin · crackedRIGHT WING OUTBOARD MOST LEADING EDGE SKIN PANEL IS CRACKED IN LINE WITH THE #10 SLAT OUTBOARD MAIN TRACK. REPAIRED RIGHT WING OUTBOARD MOST LEADING EDGE SKIN PANEL IAW B757 SRM 57-41-01-2R FIG. 201 SHEETS 4 & 5, AND 51-70-07-0G.SDR FDEA202105251398Girt Bar · out of positionLEFT EVACUATION SLIDE LIGHT WILL NOT ARM REPOSITIONED GIRT BAR, ARMED DOOR AND SLIDE LIGHT ILLUMINATES, REF AMM 25-66-10-02. OK FOR SERVICESDR FDEA2020031760578Power Supply · inoperativeFOUND DURING PREFLIGHT, INTERIOR EMERGENCY LIGHT ABOVE L1 DR INOP. REMOVED AND REPLACED M731 POWER SUPPLY PER MM 33-51-07-2, OPS CK GOOD. CLEARED MEL. OK FOR SERVICE.SDR FDEA2020031760577Power Supply · inoperativeFOUND DURING PREFLIGHT, EXTERIOR EMERGENCY SLIDE LIGHT AFT OF L1 DR INOP REMOVED AND REPLACED M731 POWER SUPPLY PER MM 33-51-07-2, OPS CK GOOD. CLEARED MEL. OK FOR SERVICE.SDR FDEA201905311198Battery Pack · failedEXTERIOR EMERGENCY LIGHT INOP ON THE RIGHT SIDE. REMOVED AND REPLACED RIGHT HAND EMERGENY LIGHT BATTERY PACK PER AMM 33-51-07- 2 OPS CHECKS GOOD. A/C OK FOR SERVICE.SDR FDEA2019060311197Battery Pack · failedALL THE RIGHT EMERGENCY LIGHTS ARE INOP REMOVED AND REPLACED RIGHT HAND EMERGENY LIGHT BATTERY PACK PER AMM 33-51-07- 2 OPS CHECKS GOOD. A/C OK FOR SERVICE.SDR FDEA201810062807Holder · wornRT FWD DOOR EXT EMERGENCY LIGHT FAILS TEST. NOTED BULB ELECTRICAL CONTACT POINT WORN CAUSING INTERMITTENT BULB OPERATION, NEEDS NEW LIGHT ASSY. REMOVED & REPLACED LAMP HOLDER ASSY AS REQUIRED, P/N= 31-4964-5, S/N=N/A, GRND CKS NORMAL, REF AMM 33-51-06.SDR FDEA201706301787Relay · malfunctionedON A 5 MILE FINAL INTO KFAR WE HAD AN AIR GRND SYSTEM EICAS, UNSAFE MAIN CARGO DOOR INDICATION, AUTO BRAKE EICAS, LEFT AND RIGHT REV ISOLATION VALVE EICAS, ALONG WITH RED REV INDICATIONS ABOVE EPR INDICATOR, COMM 1 FAILURE, STANDBY ATT FAIL, AND LANDING GSDR FDEA201704151203Bottle · blownL1 DOOR BOTTLE BLOWN. R & R THE POWER RESERVOIR IAW AMM 52-11-30-4, AND 52-11-30-6-0. AIRCRAFT OK FOR SERVICE.SDR FDEA201704151202Slide · partial deployON RAMP L1 DOOR WAS REOPENED AFTER BEING CLOSED. SLIDE WAS CAUGHT ON STRAIGHT POST WHEN REOPENED AND PARTIALLY DEPLOYED. L1 DOOR BOTTLE DISCHARGED. RESTOWED SLIDE IN REF TO AMM 25-66-01-4. BOTTLE BLOWN SO PLACED ON MEL.SDR FDEA201703030770Apu · making metalAPU FAILED IN FLIGHT. RESET, AND IT FAILED AGAIN. ATTEMPTED RUN/LEAK CHECK, APU WOULD NOT RUN. INTEROGATED ECU AND FOUND LOW OIL PRESSURE FAULT AGAIN. INSPECTED GEAR BOX MAGNETIC CHIP DETECTOR IAW AMM 49-27-04-2, FOUND METAL SHAVINGS. REINSTALLED MCD. RESDR FDEA201702140553Socket · corrodedDURING PREFLIGHT CHECK FOUND R-1 DOOR EXTERIOR EMERGENCY LIGHT INOP. FOUND DIRT AND LIGHT CORROSION IN SOCKET. CLEANED AND RELAMPED REF 33-51-06-2-1 SWPM. LIGHT CHECKS GOOD AT THIS TIME.SDR FDEA201608042811Warning System · false activationON FINAL APPROACH, WHEN SELECTING FLAPS FROM 20 TO 25 RECEIVED A T/E FLAP DISAGREE, COMPLETED QRH PROCEDURE. PERFORMED FLAPS 20 LANDING. CONTINUED PROBLEM ON GROUND. TROUBLESHOT IAW FIM 27-51 FAULT TREES 808 AND 803, COMPLYING WITH FSEU BITE PROCEDURES. SDR FDEA201605191664Skin · dentedFUSELAGE EXTERIOR SKIN LT SIDE, THERE IS AN EXISTING DENT. COMPLIED WITH PART 1 OF EA F-5310-T0324962A. REPAIR CLASSIFIED AS MAJOR.SDR FDEA201605101523Skin · unknownFUSELAGE EXTERIOR SKIN THERE IS A RIVET THAT IS NOT FLUSH AT BS 1520, BETWEEN STRINGER 29 LT & 29 RT. REPAIR CARRIED OUT IAW EA F-5330-T0324711B PART 1. REPAIR CLASSIFIED AS MAJOR.SDR FDEA201605101522Skin · damagedFUSELAGE EXTERIOR SKIN THERE IS A RIVET WITH AN ELONGATED HOLE AT BS 1600 - 1620, BETWEEN STRINGER 29 LT & 29 RT. REPAIR CARRIED OUT IAW EA F-5330-T0325043A PART 1. REPAIR CLASSIFIED AS MAJOR.SDR FDEA201605081512Skin · chafedLEFT WING LOWER INTERSPAR SKIN, EXTERIOR SURFACE FOUND CHAFING MARK AT FUEL TANK PANEL 541CB. CUT OUT BOTH FWD & AFT AREA, ALONG NR 1 PYLON UPPER INBD EDGE. LT WING LOWER INTERSPAR SKIN EXTERIOR SURFACE CHAFING MARK REMOVED & COMPLETED IAW EA F-5730-T0324554SDR FDEA201604281410Skin · dentedFUSELAGE-EXTERIOR SKIN RT SIDE, THERE IS AN EXISTING DENT WITH PREVIOUS OPERATORS STICKERS AT BS 1700 - 1720 FROM STRINGER 16 - 17. THE DENT FOUND TO EXIST ON THE DISTANCE LESS THAN 0.500 INCHES FROM THE STRINGER WHICH IS OUT OF CRITERIA IAW SRM 53-00-01-1A FSDR FDEA201604271379Skin · chafedRIGHT WING UPPER INTER SPAR SKIN, UPPER SURFACE FOUND CHAFE MARK AT WBL 76 - 78, 16" LONG FROM SKIN TE, WING TO BODY FAIRING MATING AREA. COMPLIED WITH EA F-5730-T0324272 A PT 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201604241367Intercostal · corrodedAFT CARGO COMPARTMENT NR 2 CARGO DOOR, STATION 1400, STRINGER 26R - 27R, VERTICAL INTERCOSTAL WEB HAS CORROSION. R & R WITH NEW VERTICAL INTERCOSTAL WEB IAW SRM 51-40-02 REV 117 & DWG 146N6603 SHT 07 REV K. REPAIR CLASSIFIED AS MAJOR.SDR FDEA201604241366Skin · damagedFUSELAGE EXTERIOR SKIN RT SIDE THERE IS A NEW LIGHTNING STRIKE AT BS 660 - 680, FROM STRINGER 28 - BL 0. EXTERIOR SKIN LIGHTNING STRIKE REMOVED, FOUND OUT OF LIMIT IAW SRM 53-00-01 FIG 101 DETAIL II REV 117 & REPAIR CARRIED OUT IAW EA F-5330-T0324901 PART 1. SDR FDEA201604241365Skin · damagedFUSELAGE EXTERIOR SKIN RT SIDE THERE IS A NEW LIGHTNING AT BS 680 - 660, FROM STRINGER 20 - BL 0. EXTERIOR SKIN LIGHTNING STRIKE REMOVED FOUND OUT OF LIMIT IAW SRM 53-00-01 FIG 101 DETAIL II REV 117 & REPAIR CARRIED OUT IAW EA F-5330-T0324901 PART 1 TITLE: FUSDR FDEA201604241364Skin · damagedFUSELAGE EXTERIOR SKIN RT SIDE THERE IS A NEW LIGHTNING STRIKE AT BS 680 - 660, FROM STRINGER 28 TO BL 0. EXTERIOR SKIN LIGHTNING STRIKE REMOVED, FOUND OUT OF LIMIT IAW SRM 53-00-01 FIG 101 DETAIL 11 REV 117. REPAIR CARRIED OUT IAW EA F-5330-T0324901 PART 1.SDR FDEA201604191259Beam · dentedAFT CARGO COMPARTMENT NR 2 CARGO DOOR LOWER EDGE BEAM HAS DENT. R & R WITH NEW LOWER EDGE BEAM IAW EA F-5230-T0324688 P1. REPAIR CLASSIFIED AS MAJOR.SDR FDEA201604191257Seal Depressor · dentedAFT CARGO COMPARTMENT NR 2 CARGO DOOR LOWER FWD CORNER SEAL DEPRESSOR HAS DENT.SDR FDEA201604191256Seal Depressor · dentedAFT CARGO COMPARTMENT NR 2 CARGO DOOR LOWER AFT CORNER SEAL DEPRESSOR HAS DENT.SDR FDEA201604141211Frame · corrodedCABIN STATION 1020, STRINGER 16L - 17L, FRAME AFT EDGE FOUND CORROSION. COMPLIED WITH EA F-5310-T0324712 PART 1. REPAIR FOR CORROSION ON HORIZONTAL FLANGE OF 144N8614-25 INBD CHORD. REPAIR CLASSIFIED AS MAJOR.
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