N118FE
Service difficulty reports · 55
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 = 'N118FE' 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 = 'N118FE' 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 FDEA202607170939Seat Track · damagedDURING UNLOADING, RAMP CREW REPORTED THE MDC LOCK (ID: H373) FLOOR SEAT TRACK IS BROKEN. CAN NO RESTRICTION REF EA H-5321-T0387977 MDC LOCK ID H373 BS 500 FLOOR TRACK FITTING DAMAGED EA: H-5321-T0387977 PART 1 SRM: 53-00-52-1A REF SRM 53-00-52-1A, COMPSDR FDEA202511182189Structure · no discrepancyWE HEARD A LOUD BANG IN FLIGHT AT THE TOP OF DESCENT. THE SAME NOISE OCCURRED SEVERAL MORE TIMES AT THE BEGINNING OF EACH DESCENT. UPON INSPECTION AFTER LANDING, THE DEMI CAN IN POSITION 7D WAS NOT PROPERLY SECURED AND IT WAS SLIDING BACK AND FORTH DURINGSDR FDEA202404180467Valve · failedWHILE WE WERE AWAITING TAKEOFF CLEARANCE WITH THE PARKING BRAKE SET, RECEIVED A MASTER CAUTION WITH A R HYD QTY EICAS MESSAGE FOLLOWED BY A R HYD PRIM PUMP EICAS MESSAGE. ACTIVATED THE STATUS PAGE AND WITNESSED THE RIGHT HYDRAULIC RESERVOIR QUANTITY DROP SDR FDEA202401260114Circuit Card · inoperativeSPEED BRAKES SEGMENT LIGHT & SPREED BRAKES EXT EICAS MESSAGE ILLUMINATED AFTER TAKEOFF BELOW 1000FT. AFTER ARRIVAL, ACFT CAUTION MSG EICAS & SPEED BRAKES ANNUNCIATOR LIGHT ILLUM. R & R LANDING CONFIG WARNING CARD (M983) OPS TEST OK IAW AMM 31-51-04-4. CONSDR FDEA202311251896Access Door · crackedLOWER HALF OF FUSELAGE, ACCESS DOOR 113AL WITH A BIRD STRIKE ON EXTERNAL SURFACE. THE DAMAGE AT EXTERNAL SURFACE IN ACCESS DOOR 113AL WAS REPAIRED. I.A.W. DRAWING 141T6401 REV.L I.A.W. SRM 51-40-02-0G REV.87 AUG 15,2023.SDR FDEA202311241891Skin · dentedLOWER HALF OF FUSELAGE, BETWEEN STA 135.5 AND STA 148.5, AND BETWEEN STGR 21R AND STGR 30R, BIRD STRIKE. DAMAGE AT LOWER HALF OF FUSELAGE, BETWEEN STA 135.5 AND STA 148.5, AND BETWEEN STGR 21R AND STGR 30R WAS REPAIRED. I.A.W. E.A.#: H-5330-T0377079 PART: SDR FDEA202311241890Skin · crackedUPPER HALF OF FUSELAGE, BETWEEN STA 132.5 AND STA 143.5, AND BETWEEN STGR 14-L AND STGR 18-L, BIRD STRIKE. DAMAGE AT UPPER HALF OF FUSELAGE, BETWEEN STA 132.5 AND STA 143.5, AND BETWEEN STGR 14-L AND STGR 18-L WAS REPAIRED. I.A.W. E.A.#: H-5330- T0377062 PSDR FDEA202311241889Skin · damagedLOWER HALF OF FUSELAGE, BETWEEN STA 132.5 AND 143.5, AND BETWEEN STGR 30-L AND STGR 31-L, BIRD STRIKE. DAMAGE AT LOWER HALF OF FUSELAGE, BETWEEN STA 132.5 AND BETWEEN STGR 50-L AND STGR 31-L, WAS REPAIRED I.A.W. E.A.:# H-5330-T0377078 PART: 1(P1) RELEASESDR FDEA202308021344Unknown · unknownESCAPE ROPE FOR CREW ENTRY DOOR IS PARTIALLY OUT OF ITS POCKET JAMMING THE DOOR. REINSTALLED EMERGENCY ECSAPE ROPE AS REQUIRED IAW MM 25-61-04-2-1. OK FOR SERVICESDR FDEA202304150655Flap · unknownFOUND DENT ON RH INBOARD TRAILING EDGE FLAP TOPSIDE. REPAIRED RT WING- INBOARD FLAP UPPER SKIN TOP SURFACE TRAILING EDGE DENT AT LOCATION INBD FLAP TRAILING EDGE TOP SURFACE 39 INCHES FROM INB EDGE 9.5 INCHES WITH A 2 IN. CIRCLE REPAIR, IN REF. TO 767 SRMSDR FDEA202206061384Slat · dentedRH WING SLAT # 8 WITH 11 DENTS IN UPPER WEDGE AREA RH WING SLAT # 8 WITH 14 DENTS WERE EVALUATED AND FOUND WITHIN LIMITS IAW SRM MAXIMIM DIMENSION L= 1.600" W=0.600". DENT ON OSS 445.35 WAS REPAIRED IAW B767 SRM 57- 43-02-1A PAG. 1-6 FIG. 101 (SHEET 3) NOTESDR FDEA202206041375Flap · delaminatedRIGHT WING OUTBOARD FLAP LEADING EDGE WITH DELAMINATION WBL: 414. RIGHT WING OUTBOARD FLAP LEADING EDGE WBL 414 WAS REPAIRED IAW B767 SRM 57-53-01-2R REP. 1 PAG. 1-9 FIG. 201 (SHEET 5) TABLE I AND B767 SRM 51-70-17-0G PAR. 4.A. FIG. 10 REV. 82 DEC15/2021SDR FDEA202206041374Slat · dentedLEFT WING SLAT NO 5 DENT IN UPPER WEDGE AREA WS. 433.1 LEFT WING SLAT NO 5 DENT IN UPPER WEDGE AREA WS 433.1 THAT WAS REPAIRED I.A.W. SRM 57- 43-02-2R FIG. 201 SHEET 1 AND SRM B767 51-70-10-2R PAGE 149, 157 FIG. 202 SHEET 3 REV. 82 DEC15/2021SDR FDEA202204160978Former · crackedCRACKED FORMER ON LS PN: 114T2170-5/WITH ANGLE 114T 2171-4; LOOSE/DAMAGED FASTENERS LOCATED AT LS FLE OSS 441 ALSO. 0000452710 : ROSNER, DANIEL D - 17-APR-2022 03:18 REMOVED THE DAMAGED FORMER AND ANGLE LOCATED AT LH WING STATION OSS 441.596. AND INSTALLED SDR FDEA202103290794Slat · gougedRIGHT WING #8 SLAT, UPPER TRAILING EDGE, LOWER FACE IS GOUGED AT OUTBOARD AUX TRACK. REPAIRED RIGHT WING #8 SLAT UPPER TRAILING EDGE LOWER FACE GOUGED AT OUTBOARD AUX TRACK IAW B767 SRM 57-43- 02-2R-1 DETAIL 1 AND SRM 51-70-10-2R REPAIR GENERALSDR FDEA202103230756Floor Panel · damagedMAIN DECK FLOOR PANEL 242SFF IS PUNCTURED & HAS EDGE DAMAGE REPAIRED FLOOR PANEL IAW B767 SRM 53-00-50-2RSDR FDEA202103230755Floor Panel · damagedMAIN DECK FLOOR PANEL 241KFF IS PUNCTURED REPAIRED FLOOR PANEL IAW B767 SRM 53-00-50-2RSDR FDEA202103230754Floor Panel · damagedMAIN DECK FLOOR PANEL 241YFA IS PUNCTURED & HAS EDGE DAMAGE REPAIRED FLOOR PANEL IAW B767 SRM 53-00-50-2RSDR FDEA202103230753Floor Panel · delaminatedMAIN DECK FLOOR PANEL 242UFF IS DELAMINATED ON FWD END REPAIRED FLOOR PANEL IAW B767 SRM 53-00-50-2RSDR FDEA202103230752Floor Panel · damagedMAIN DECK FLOOR PANEL 241FFF DENTED REPAIRED FLOOR PANEL IAW B767 SRM 53-00-50-2RSDR FDEA202103230751Floor Panel · damagedMAIN DECK FLOOR PANEL 241BFF HAS DAMAGED INSERT REMOVED & REPLACED INSERT IAW B767 SRM 53-00-50-2R & FEDEX DRAWING SRZ-25-005, REV RSDR FDEA202103210735Strap · crackedLEFT WING LEADING EDGE SPLIC STRAP IS CRACKED REMOVED & REPLACED STRAP IAW BAC DWG 114T2800 REV CSDR FDEA202103210734Strap · crackedRH WING LEADING EDGE SPLICE STRAP IS CRACKED REMOVED & REPLACED STRAP IAW BAC DWG 114T2800 SHT 6 REV CSDR FDEA202103210736Shear Tie · cracked#2 PYLON, INBD SHEAR TIE @ NAC STA 303 IS CRACKED REMOVED & REPLACED SHEAR TIE IAW BAC DWG 313T2310 REV -SDR FDEA202103200711Heat Shield · crackedTAIL SECTION , INTERNAL , APU BLEED AIR DUCT HEAT SHIELD IS CRACKED AT THE UPPER AFT ATTACH FASTENER HOLE IN THE L/H STABILIZER TORSION BOX AREA BELOW THE THS JUST AFT OF STA 1725.5 REPAIRED DAMAGE ON HEAT SHIELD IAW EA# H-3610-T0360506SDR FDEA202103190710Floor Support · crackedL/H NOSE TUNNEL MAIN CABIN FLOOR SUPPORT STRUCTURAL VERTICAL ANGLE IS CRACKED AT STA 246 APROX LBL50 REMOVED AND REPLACED ANGLE IAW BAC DRAWING 141T5146, REV BSDR FDEA202103190709Attach Angle · crackedAFT PIT, FWD OF PIT STA 1087 LBL20 FLOOR SUPPORT STRUCTURE VERTICAL ATTACH ANGLE UPPER SIDE IS CRACKED REMOVED AND REPLACED AFT PIT , FWD OF AFT PIT STA 1087 LBL20 FLOOR SUPPORT STRUCTURE VERTICAL ATTACH ANGLESDR FDEA202103190708Floor Support · crackedAFT PIT , FWD OF AFT COMP. STA 1087 RBL20 FLOOR SUPPORT STRUCTURE VERTICAL ATTACH CLIP UPPER SIDE IS CRACKED REMOVED AND REPLACED AFT PIT , FWD OF AFT COMPT. STA 1087 RBL20 FLOOR SUPPORT STRUCTURE VERTICAL ATTACH CLIPSDR FDEA202103190704Tube · crackedBULK DOOR COMPARTMENT DOOR COUNTER BALANCE SPRING TUBE IS CRACKED REMOVED AND REPLACED BULK DOOR COUNTER BALANCE SPRING TUBE PER B767 AMM 52-36- 02-5SDR FDEA202103180698Shear Tie · crackedNO.1 PYLON, INBD SIDE, NAC STA 303 SHEAR TIE IS CRACKED REMOVED & REPLACED SHEAR TIE IAW BAC DWG 313T2310SDR FDEA202103180699Shear Tie · crackedNO.1 PYLON, INBD SIDE, NAC STA 303 HAS CRACKED SHEAR TIE REMOVED & REPLACED SHEAR TIE IAW BAC DWG 313T2310SDR FDEA202103180690Panel · crackedLEFT WING, LEADING EDGE , FUELING PANEL 521 QB , WEB IS CRACKED REPAIRED WEB BEHIND 521 QB IAW B767 SRM 57-41-13-2R , B767 SRM 51-20-01 AND B767 AMM 52-49- 04-4SDR FDEA202103170682Former · crackedLEFT WING NOSE FORMER & ANGLE CRACKED @ OSS 441 REMOVED & REPLACED FORMER & ANGLE ASSY IAW BAC DWG 114T2241REV - & FEDEX EA H- 5720-T0360399-P1SDR FDEA202103140647Former · crackedLH WING LEADING EDGE NOSE FORMER IS CRACKED @ OSS 499 REMOVED & REPLACED FORMER IAW BAC DWG 114T2161 REV - & FEDEX EA H-5720-T0360398-P1SDR FDEA202103140646Bracket · crackedRIGHT WING FUELING STATION DOOR LIGHT HOUSING BRACKET IS CRACKED REMOVED & REPLACED BRACKET IAW B767 AMM 52-49-04SDR FDEA202103140645Frame Angle · cracked#1 PYLON, NAC STA 377, OUTBD FRAME CLIP IS CRACKED REMOVED & REPLACED CLIP IAW BAC DWG 313T3380 REV FSDR FDEA202103140644Frame Angle · cracked#1 PYLON, NAC STA 377, INBD FRAME CLIP IS CRACKED REMOVED & REPLACED CLIP IAW BAC DWG 313T3380 REV FSDR FDEA202103140643Frame Angle · cracked#2 PYLON, NAC STA 377, OUTBD FRAME CLIP IS CRACKED REMOVED & REPLACED CLIP IAW BAC DWG 313T3380 REV FSDR FDEA202103140642Frame Angle · cracked#2 PYLON, NAC STA 377, INBD SIDE, FRAME CLIP CRACKED REMOVED & REPLACED CLIP IAW BAC DWG 313T3380 REV FSDR FDEA202103120625Bracket · crackedRH WING TORQUE TUBE GUIDE BRACKET CRACKED @ LES 285 REMOVED & REPLACED BRACKET IAW BAC DWG 114T1240 REV -SDR FDEA202103120624Bracket · crackedLH WING TORQUE TUBE GUIDE BRACKET CRACKED LES 285 REMOVED & REPLACED BRACK IAW BAC DWG 114T1240 REV -SDR FDEA2020082521988Rod · damagedDURING ACCOMPLISHMENT OF FEA H-3243-F0356064, FOUND #6 MLG BRAKE ROD NEED TO BE DISASSEMBLE AND PROPERLY REASSEMBLE TO BRAKE ATTACHMENT JOINT DISASSEMBLED AND REASSEMBLED #6 MLG BRAKE ROD TO BRAKE ATTACHMENT JOINT REF AMM 32-11-20-4-4. A/C OK TO CONTISDR FDEA2020082521987Rod · damagedDURING ACCOMPLISHMENT OF FEA H-3243-F0356064, FOUND #5 MLG BRAKE ROD NEED TO BE DISASSEMBLE AND PROPERLY REASSEMBLE TO BRAKE ATTACHMENT JOINT DISASSEMBLED AND REASSEMBLED #5 MLG BRAKE ROD TO BRAKE ATTACHMENT JOINT REF AMM 32-11-20-4-4. A/C OK TO CONTISDR FDEA2020082521986Rod · damagedDURING ACCOMPLISHMENT OF FEA H-3243-F0356064, FOUND #2 MLG BRAKE ROD NEED TO BE DISASSEMBLE AND PROPERLY REASSEMBLE TO BRAKE ATTACHMENT JOINT DISASSEMBLED AND REASSEMBLED #2 MLG BRAKE ROD TO BRAKE ATTACHMENT JOINT REF AMM 32-11-20-4-4. A/C OK TO CONSDR FDEA2020082521985Rod · damagedDURING ACCOMPLISHMENT OF FEA H-3243-F0356064, FOUND NR 4 MLG BRAKE ROD NEED TO BE DISASSEMBLE AND PROPERLY REASSEMBLE TO BRAKE ATTACHMENT JOINT. DISASSEMBLED AND REASSEMBLED THE NR 4 MLG BRAKE ROD TO BRAKE ATTACHMENT JOINT IAW AMM 32-11-20-4-4. ACFT OK SDR FDEA202002070279Pump · malfunctioned20 MINUTES INTO FLIGHT GOT FUEL CONFIG ALERT. RETURNED TO KMEM. FUEL NOT FEEDING FROM LEFT TANK. REMOVED AND REPLACED THE L/H AFT BOOST PUMP IN REF. TO B767 AMM. 28-22-032-4. OPS AND LEAK TEST NORMAL.SDR FDEA202002040260Pump · malfunctioned20 MINUTES INTO FLIGHT GOT FUEL CONFIG ALERT. RETURNED TO KMEM. FUEL NOT FEEDING FROM LEFT TANK. CHANGED LEFT AND RIGHT BOOST PUMPS MPN 5006003D. REMOVED AND REPLACE THE LT AFT BOOST PUMP, IN REF TO B767 AMM 28-22-032-4. OPS AND LEAK TEST NORMAL.SDR FDEA201912240001Skin · damagedFUSELAGE HAS IMPACT DAMAGE AT STA 1109 AT STR 4L REPAIRED FUSELAGE SKIN PER E.A. H-5330-T0351626 PART 1.SDR FDEA201909132268Pump · leakingAPPROX 2HRS INTO FLT, EICAS ALERT 'L HYD QTY', LT HYD QTY SLOWLY DECREASED FROM ABOVE 0.9 TO 0.01 WITH 'RF' INDICATED. EICAS ALERT 'HYD PRIM PUMP' DISPLAYED SHORTLY THEREAFTER QRH COMPLIED WITH AND LT ENG PRIMARY PUMP SELECTED 'OFF'. LT HYD PRESS STAYED IN NOSDR FDEA2019080871812Wedge · gougedLEFT WING #5 SLAT TRAILING EDGE WEDGE GOUGED REPAIRED DAMAGED IAW EA# H-2780-T0348663 - P1 FLIGHT CONTROL- L/E SLATS-#5 SLAT, TRAILING EDGE SKIN- GOUGE GOUGE-RSC SRM REPAIR TRACKING
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