# Service difficulty reports: N118FE A list on [N118FE](https://openairdocs.org/aircraft/N118FE.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. Page 1 of 2 · 55 reports - [SDR FDEA202607170939](https://openairdocs.org/sdr/FDEA202607170939.md): Seat Track · damaged · Jul 17, 2026 · N118FE · Boeing 7673S2F · Fuselage, Seat/Cargo Attach Fittings > DURING 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, COMP - [SDR FDEA202511182189](https://openairdocs.org/sdr/FDEA202511182189.md): Structure · no discrepancy · Nov 18, 2025 · N118FE · Boeing 7673S2F · Fuselage Structure (General) > WE 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 DURING - [SDR FDEA202404180467](https://openairdocs.org/sdr/FDEA202404180467.md): Valve · failed · Apr 18, 2024 · N118FE · Boeing 7673S2F · Hydraulic System, Main > WHILE 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 FDEA202401260114](https://openairdocs.org/sdr/FDEA202401260114.md): Circuit Card · inoperative · Jan 26, 2024 · N118FE · Boeing 7673S2F · Landing Gear System > SPEED 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. CON - [SDR FDEA202311251896](https://openairdocs.org/sdr/FDEA202311251896.md): Access Door · cracked · Nov 25, 2023 · N118FE · Boeing 767300 · Fuselage Main, Plate/Skin > LOWER 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 FDEA202311241891](https://openairdocs.org/sdr/FDEA202311241891.md): Skin · dented · Nov 24, 2023 · N118FE · Boeing 767300 · Fuselage Main, Plate/Skin > LOWER 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 FDEA202311241890](https://openairdocs.org/sdr/FDEA202311241890.md): Skin · cracked · Nov 24, 2023 · N118FE · Boeing 767300 · Fuselage Main, Plate/Skin > UPPER 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 P - [SDR FDEA202311241889](https://openairdocs.org/sdr/FDEA202311241889.md): Skin · damaged · Nov 24, 2023 · N118FE · Boeing 767300 · Fuselage Main, Plate/Skin > LOWER 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) RELEASE - [SDR FDEA202308021344](https://openairdocs.org/sdr/FDEA202308021344.md): Unknown · unknown · Aug 2, 2023 · N118FE · Boeing 767300 · Emergency Equipment > ESCAPE 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 SERVICE - [SDR FDEA202304150655](https://openairdocs.org/sdr/FDEA202304150655.md): Flap · unknown · Apr 15, 2023 · N118FE · Boeing 767300 · Trailing Edge Flap Control System > FOUND 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 SRM - [SDR FDEA202206061384](https://openairdocs.org/sdr/FDEA202206061384.md): Slat · dented · Jun 6, 2022 · N118FE · Boeing 767300 · Leading Edge Devices > RH 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) NOTE - [SDR FDEA202206041375](https://openairdocs.org/sdr/FDEA202206041375.md): Flap · delaminated · Jun 4, 2022 · N118FE · Boeing 767300 · Trailing Edge Flaps > RIGHT 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 DEC15/2021 - [SDR FDEA202206041374](https://openairdocs.org/sdr/FDEA202206041374.md): Slat · dented · Jun 4, 2022 · N118FE · Boeing 767300 · Leading Edge Devices > LEFT 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 DEC15/2021 - [SDR FDEA202204160978](https://openairdocs.org/sdr/FDEA202204160978.md): Former · cracked · Apr 16, 2022 · N118FE · Boeing 7673S2F · Wing Miscellaneous Structure > CRACKED 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 FDEA202103290794](https://openairdocs.org/sdr/FDEA202103290794.md): Slat · gouged · Mar 29, 2021 · N118FE · Boeing 7673S2F · Leading Edge Devices > RIGHT 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 GENERAL - [SDR FDEA202103230756](https://openairdocs.org/sdr/FDEA202103230756.md): Floor Panel · damaged · Mar 23, 2021 · N118FE · Boeing 7673S2F · Fuselage Floor Panel > MAIN DECK FLOOR PANEL 242SFF IS PUNCTURED & HAS EDGE DAMAGE REPAIRED FLOOR PANEL IAW B767 SRM 53-00-50-2R - [SDR FDEA202103230755](https://openairdocs.org/sdr/FDEA202103230755.md): Floor Panel · damaged · Mar 23, 2021 · N118FE · Boeing 7673S2F · Fuselage Floor Panel > MAIN DECK FLOOR PANEL 241KFF IS PUNCTURED REPAIRED FLOOR PANEL IAW B767 SRM 53-00-50-2R - [SDR FDEA202103230754](https://openairdocs.org/sdr/FDEA202103230754.md): Floor Panel · damaged · Mar 23, 2021 · N118FE · Boeing 7673S2F · Fuselage Floor Panel > MAIN DECK FLOOR PANEL 241YFA IS PUNCTURED & HAS EDGE DAMAGE REPAIRED FLOOR PANEL IAW B767 SRM 53-00-50-2R - [SDR FDEA202103230753](https://openairdocs.org/sdr/FDEA202103230753.md): Floor Panel · delaminated · Mar 23, 2021 · N118FE · Boeing 7673S2F · Fuselage Floor Panel > MAIN DECK FLOOR PANEL 242UFF IS DELAMINATED ON FWD END REPAIRED FLOOR PANEL IAW B767 SRM 53-00-50-2R - [SDR FDEA202103230752](https://openairdocs.org/sdr/FDEA202103230752.md): Floor Panel · damaged · Mar 23, 2021 · N118FE · Boeing 7673S2F · Fuselage Floor Panel > MAIN DECK FLOOR PANEL 241FFF DENTED REPAIRED FLOOR PANEL IAW B767 SRM 53-00-50-2R - [SDR FDEA202103230751](https://openairdocs.org/sdr/FDEA202103230751.md): Floor Panel · damaged · Mar 23, 2021 · N118FE · Boeing 7673S2F · Fuselage Floor Panel > MAIN DECK FLOOR PANEL 241BFF HAS DAMAGED INSERT REMOVED & REPLACED INSERT IAW B767 SRM 53-00-50-2R & FEDEX DRAWING SRZ-25-005, REV R - [SDR FDEA202103210735](https://openairdocs.org/sdr/FDEA202103210735.md): Strap · cracked · Mar 21, 2021 · N118FE · Boeing 7673S2F · Wing Miscellaneous Structure > LEFT WING LEADING EDGE SPLIC STRAP IS CRACKED REMOVED & REPLACED STRAP IAW BAC DWG 114T2800 REV C - [SDR FDEA202103210734](https://openairdocs.org/sdr/FDEA202103210734.md): Strap · cracked · Mar 21, 2021 · N118FE · Boeing 7673S2F · Wing Miscellaneous Structure > RH WING LEADING EDGE SPLICE STRAP IS CRACKED REMOVED & REPLACED STRAP IAW BAC DWG 114T2800 SHT 6 REV C - [SDR FDEA202103210736](https://openairdocs.org/sdr/FDEA202103210736.md): Shear Tie · cracked · Mar 21, 2021 · N118FE · Boeing 7673S2F · Nacelle/Pylon, Main Frame > #2 PYLON, INBD SHEAR TIE @ NAC STA 303 IS CRACKED REMOVED & REPLACED SHEAR TIE IAW BAC DWG 313T2310 REV - - [SDR FDEA202103200711](https://openairdocs.org/sdr/FDEA202103200711.md): Heat Shield · cracked · Mar 20, 2021 · N118FE · Boeing 7673S2F · APU Cowling/Containment > TAIL 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-T0360506 - [SDR FDEA202103190710](https://openairdocs.org/sdr/FDEA202103190710.md): Floor Support · cracked · Mar 19, 2021 · N118FE · Boeing 7673S2F · Fuselage Miscellaneous Structure > L/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 B - [SDR FDEA202103190709](https://openairdocs.org/sdr/FDEA202103190709.md): Attach Angle · cracked · Mar 19, 2021 · N118FE · Boeing 7673S2F · Fuselage Miscellaneous Structure > AFT 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 ANGLE - [SDR FDEA202103190708](https://openairdocs.org/sdr/FDEA202103190708.md): Floor Support · cracked · Mar 19, 2021 · N118FE · Boeing 7673S2F · Fuselage Miscellaneous Structure > AFT 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 CLIP - [SDR FDEA202103190704](https://openairdocs.org/sdr/FDEA202103190704.md): Tube · cracked · Mar 19, 2021 · N118FE · Boeing 767330 · Cargo/Baggage Doors > BULK DOOR COMPARTMENT DOOR COUNTER BALANCE SPRING TUBE IS CRACKED REMOVED AND REPLACED BULK DOOR COUNTER BALANCE SPRING TUBE PER B767 AMM 52-36- 02-5 - [SDR FDEA202103180698](https://openairdocs.org/sdr/FDEA202103180698.md): Shear Tie · cracked · Mar 18, 2021 · N118FE · Boeing 7673S2F · Nacelle/Pylon, Main Frame > NO.1 PYLON, INBD SIDE, NAC STA 303 SHEAR TIE IS CRACKED REMOVED & REPLACED SHEAR TIE IAW BAC DWG 313T2310 - [SDR FDEA202103180699](https://openairdocs.org/sdr/FDEA202103180699.md): Shear Tie · cracked · Mar 18, 2021 · N118FE · Boeing 7673S2F · Nacelle/Pylon, Main Frame > NO.1 PYLON, INBD SIDE, NAC STA 303 HAS CRACKED SHEAR TIE REMOVED & REPLACED SHEAR TIE IAW BAC DWG 313T2310 - [SDR FDEA202103180690](https://openairdocs.org/sdr/FDEA202103180690.md): Panel · cracked · Mar 18, 2021 · N118FE · Boeing 7673S2F · Wing Main, Frame Structure > LEFT 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- 04-4 - [SDR FDEA202103170682](https://openairdocs.org/sdr/FDEA202103170682.md): Former · cracked · Mar 17, 2021 · N118FE · Boeing 7673S2F · Wing Main, Frame Structure > LEFT WING NOSE FORMER & ANGLE CRACKED @ OSS 441 REMOVED & REPLACED FORMER & ANGLE ASSY IAW BAC DWG 114T2241REV - & FEDEX EA H- 5720-T0360399-P1 - [SDR FDEA202103140647](https://openairdocs.org/sdr/FDEA202103140647.md): Former · cracked · Mar 14, 2021 · N118FE · Boeing 7673S2F · Wing Main, Frame Structure > LH WING LEADING EDGE NOSE FORMER IS CRACKED @ OSS 499 REMOVED & REPLACED FORMER IAW BAC DWG 114T2161 REV - & FEDEX EA H-5720-T0360398-P1 - [SDR FDEA202103140646](https://openairdocs.org/sdr/FDEA202103140646.md): Bracket · cracked · Mar 14, 2021 · N118FE · Boeing 7673S2F · Wing Main, Frame Structure > RIGHT WING FUELING STATION DOOR LIGHT HOUSING BRACKET IS CRACKED REMOVED & REPLACED BRACKET IAW B767 AMM 52-49-04 - [SDR FDEA202103140645](https://openairdocs.org/sdr/FDEA202103140645.md): Frame Angle · cracked · Mar 14, 2021 · N118FE · Boeing 7673S2F · Nacelle/Pylon, Main Frame > #1 PYLON, NAC STA 377, OUTBD FRAME CLIP IS CRACKED REMOVED & REPLACED CLIP IAW BAC DWG 313T3380 REV F - [SDR FDEA202103140644](https://openairdocs.org/sdr/FDEA202103140644.md): Frame Angle · cracked · Mar 14, 2021 · N118FE · Boeing 7673S2F · Nacelle/Pylon, Main Frame > #1 PYLON, NAC STA 377, INBD FRAME CLIP IS CRACKED REMOVED & REPLACED CLIP IAW BAC DWG 313T3380 REV F - [SDR FDEA202103140643](https://openairdocs.org/sdr/FDEA202103140643.md): Frame Angle · cracked · Mar 14, 2021 · N118FE · Boeing 7673S2F · Nacelle/Pylon, Main Frame > #2 PYLON, NAC STA 377, OUTBD FRAME CLIP IS CRACKED REMOVED & REPLACED CLIP IAW BAC DWG 313T3380 REV F - [SDR FDEA202103140642](https://openairdocs.org/sdr/FDEA202103140642.md): Frame Angle · cracked · Mar 14, 2021 · N118FE · Boeing 7673S2F · Nacelle/Pylon, Main Frame > #2 PYLON, NAC STA 377, INBD SIDE, FRAME CLIP CRACKED REMOVED & REPLACED CLIP IAW BAC DWG 313T3380 REV F - [SDR FDEA202103120625](https://openairdocs.org/sdr/FDEA202103120625.md): Bracket · cracked · Mar 12, 2021 · N118FE · Boeing 7673S2F · Wing Miscellaneous Structure > RH WING TORQUE TUBE GUIDE BRACKET CRACKED @ LES 285 REMOVED & REPLACED BRACKET IAW BAC DWG 114T1240 REV - - [SDR FDEA202103120624](https://openairdocs.org/sdr/FDEA202103120624.md): Bracket · cracked · Mar 12, 2021 · N118FE · Boeing 7673S2F · Wing Miscellaneous Structure > LH WING TORQUE TUBE GUIDE BRACKET CRACKED LES 285 REMOVED & REPLACED BRACK IAW BAC DWG 114T1240 REV - - [SDR FDEA2020082521988](https://openairdocs.org/sdr/FDEA2020082521988.md): Rod · damaged · Aug 22, 2020 · N118FE · Boeing 7673S2F · Landing Gear Brake System > DURING 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 CONTI - [SDR FDEA2020082521987](https://openairdocs.org/sdr/FDEA2020082521987.md): Rod · damaged · Aug 22, 2020 · N118FE · Boeing 7673S2F · Landing Gear Brake System > DURING 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 CONTI - [SDR FDEA2020082521986](https://openairdocs.org/sdr/FDEA2020082521986.md): Rod · damaged · Aug 22, 2020 · N118FE · Boeing 7673S2F · Landing Gear Brake System > DURING 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 CON - [SDR FDEA2020082521985](https://openairdocs.org/sdr/FDEA2020082521985.md): Rod · damaged · Aug 22, 2020 · N118FE · Boeing 7673S2F · Landing Gear Brake System > DURING 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 FDEA202002070279](https://openairdocs.org/sdr/FDEA202002070279.md): Pump · malfunctioned · Feb 7, 2020 · N118FE · Boeing 7673S2F · Fuel Boost Pump > 20 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 FDEA202002040260](https://openairdocs.org/sdr/FDEA202002040260.md): Pump · malfunctioned · Feb 4, 2020 · N118FE · Boeing 7673S2F · Fuel Boost Pump > 20 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 FDEA201912240001](https://openairdocs.org/sdr/FDEA201912240001.md): Skin · damaged · Dec 24, 2019 · N118FE · Boeing 7673S2F · Fuselage Main, Plate/Skin > FUSELAGE HAS IMPACT DAMAGE AT STA 1109 AT STR 4L REPAIRED FUSELAGE SKIN PER E.A. H-5330-T0351626 PART 1. - [SDR FDEA201909132268](https://openairdocs.org/sdr/FDEA201909132268.md): Pump · leaking · Sep 13, 2019 · N118FE · Boeing 7673S2F · Hydraulic Pump (Electric/Engine), Main > APPROX 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 NO - [SDR FDEA2019080871812](https://openairdocs.org/sdr/FDEA2019080871812.md): Wedge · gouged · Aug 7, 2019 · N118FE · Boeing 7673S2F · Leading Edge Devices > LEFT 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 Next page: https://openairdocs.org/aircraft/N118FE/reports.md?page=2 ## The whole list in SQL Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS: ```sql 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 ``` This list as a web page: https://openairdocs.org/aircraft/N118FE/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.