# Service difficulty reports: N118RW, cancelled May 11, 2004 A list on [N118RW, cancelled May 11, 2004](https://openairdocs.org/deregistered/N118RW-2004-05-11.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 3 · 103 reports - [SDR FL3A200200389](https://openairdocs.org/sdr/FL3A200200389.md): Check Valve · inoperative · Nov 16, 2002 · N118RW · Boeing 7372Y5 · Pneumatic System > DURING CLIMB OUT, THE FLIGHT CREW NOTED AN ILLUMINATED WING/BODY OVERHEAT LIGHT WHICH WOULD NOT EXTINGUISH WHEN QUICK REFERENCE HANDBOOK ITEMS WERE ACCOMPLISHED. THE AIRCRAFT RETURNED TO THE DEPARTURE AIRPORT.MAINTENANCE REMOVED AND REPLACED THE START MANIFOL - [SDR F3LA200200385](https://openairdocs.org/sdr/F3LA200200385.md): Hydraulic Line · damaged · Nov 6, 2002 · N118RW · Boeing 7372Y5 · Hydraulic Power System > DURING FLIGHT, A SYSTEM HYDRAULIC QUANTITY DROPPED TO ZERO FOLLOWED BY THE FAILURE OF THE NUMBER 2 ENGINE, ENGINE DRIVEN HYDRAULIC PUMP. A SYSTEM PRESSURE REMIAINED NORMAL. ON FINAL APPROACH TO DIVERSION SITY AIRPORT, A SYSTEM PRESSURE DROPPED TO ZERO. STAN - [SDR F3LA200200265](https://openairdocs.org/sdr/F3LA200200265.md): A/C Pack · malfunctioned · Sep 25, 2002 · N118RW · Boeing 7372Y5 · Cabin Cooling System > AIR TURN BACK. FLIGHT CREW REPORTED SMOKE IN CABIN, LT WING/BODY OVERHEAT ILLUMINATED AND RT PACK TRIPPED OFF. DECLARED AN EMERGENCY AND RETURNED TO DEN. AIRCRAFT LANDED WITHOUT INCIDENT. ON APPROACH, AILERONS WERE DIFFICULT TO MOVE AND HAD A SHUDDER BELOW - [SDR F3LA200200258](https://openairdocs.org/sdr/F3LA200200258.md): Odor · detected · Sep 10, 2002 · N118RW · Boeing 7372Y5 · Air Distribution System > AIR TURNBACK. FLIGHT CREW REPORTED FWD LAVATORY SMOKE ALARM ACTIVATED WHILE CLIMBING THROUGH 8000 FT. PASSENGERS IN ROW 2 NOTED DISTINCT SMELL/ODOR OR SMOKE (OVEN/ELECTRICAL) DURING FLIGHT. NR 2 PACK TRIP OFF LIGHT ILLUMINATED IMMEDIATELY BEFORE SMOKE ALARM - [SDR F3LA200200201](https://openairdocs.org/sdr/F3LA200200201.md): Overheat Loop · out of position · Jul 26, 2002 · N118RW · Boeing 7372Y5 · Overheat Detection > DURING CLIMBOUT, THE FLIGHT CREW DISCOVERED A WIND/BODY OVERHEAT LIGHT ON. QRH ITEMS ACCOMPLISHED AND LIGHT EXTINGUISHED. AIR TURNBACK ACCOMPLISHED. UPON INSPECTION BY MAINTENANCE, AFT CARGO PIT HAD TWO AREAS WHERE THE OVERHEAT DETECTOR WAS TOUCHING THE BLE - [SDR F3LA200200152](https://openairdocs.org/sdr/F3LA200200152.md): Fire Detector · false activation · May 21, 2002 · N118RW · Boeing 7372Y5 · Fire Detection > UPON ARRIVAL AT GATE, FLIGHT CREW REPORTED THE FIRE BELL SOUNDED AND THE NR 1 ENGINE FIRE HANDLE WAS ILLUMINATED. PULLED NR 1 FIRE HANDLE AND DISCHARGED THE LEFT BOTTLE INTO THE NR 1 ENGINE. INSPECTED NR 1 ENGINE FOR EVIDENCE OF FIRE, NONE FOUND. INSPECTED - [SDR F3LA200200103](https://openairdocs.org/sdr/F3LA200200103.md): Cowling · cracked · Feb 28, 2002 · N118RW · Boeing 7372Y5 · Engine Cowling System > DURING C-3 CHECK, INSPECTION REPORTED CRACK ON AFT LOWER CORNER OF NR 2 ENGINE OUTBOARD FIXED COWL NEXT TO FIRE SEAL. FABRICATED AND INSTALLED REPAIR PER SRM 51-40-3 AND 51-30-2. - [SDR F3LA200200102](https://openairdocs.org/sdr/F3LA200200102.md): Web · corroded · Feb 28, 2002 · N118RW · Boeing 7372Y5 · Fuselage Miscellaneous Structure > DURING C-3 CHECK, INSPECTION REPORTED AFT LAVATORY FLOOR WEB CORRODED, STA 1016, AT DRAIN TO LBL 30. - [SDR F3LA200200101](https://openairdocs.org/sdr/F3LA200200101.md): Attach Angle · corroded · Feb 28, 2002 · N118RW · Boeing 7372Y5 · Fuselage Miscellaneous Structure > DURING C-3 CHECK, INSPECTION REPORTED CORROSION ON SIDEWALL PANEL ATTACH ANGLE AT STA 727, LBL 21 TO LBL 25. - [SDR F3LA200200100](https://openairdocs.org/sdr/F3LA200200100.md): Attach Angle · corroded · Feb 28, 2002 · N118RW · Boeing 7372Y5 · Fuselage Miscellaneous Structure > DURING C-3 CHECK, INSPECTION REPORTED CORROSION ON SIDEWALL ATTACH ANGLE AT STA 947.5, STR 21R TO 24R. FABRICATED AND INSTALLED REPLACEMENT ANGLE PER BOEING DRAWING 65-55726 AND SRM 51-40-3. - [SDR F3LA200200098](https://openairdocs.org/sdr/F3LA200200098.md): Clip · corroded · Feb 28, 2002 · N118RW · Boeing 7372Y5 · Fuselage Miscellaneous Structure > DURING C-3 CHECK, INSPECTION REPORTED CORROSION ON CLIP AT FWD FRAME, STA 360. FABRICATED AND INSTALLED CHANNEL TIE PER SRM 51-20-01 AND 51-30-2. - [SDR F3LA200200097](https://openairdocs.org/sdr/F3LA200200097.md): Web · corroded · Feb 28, 2002 · N118RW · Boeing 7372Y5 · Fuselage Miscellaneous Structure > DURING C-3 CHECK, INSPECTION REPORTED VERTICAL WEB CORRODED FROM STA 352 TO STA 360. FABRICATED AND INSTALLED REPLACEMENT WEB PER SRM 51-20-01 AND 51-30-2. - [SDR F3LA200200096](https://openairdocs.org/sdr/F3LA200200096.md): Stiffener · cracked · Feb 28, 2002 · N118RW · Boeing 7372Y5 · Fuselage Miscellaneous Structure > DURING C-3 CHECK, INSPECTION REPORTED STIFFENER ANGLE CRACKED AT STA 298 - STA 304. FABRICATED AND INSTALLED REPLACEMENT CLIP PER SRM 51-10-2 AND 51-30-2. - [SDR F3LA200200095](https://openairdocs.org/sdr/F3LA200200095.md): Threshold · cracked · Feb 28, 2002 · N118RW · Boeing 7372Y5 · Fuselage Miscellaneous Structure > DURING C-3 CHECK, INSPECTION REPORTED CRACK IN RADIUS UPPER SURFACE 28 INCHES FWD OF AFT EDGE OF WEB THRESHOLD C-2 DOOR AT STR 25-R, STA 794-847. REMOVED DAMAGED AREA AND INSTALLED DOUBLER AND FILLER ON WEB PER SRM 51-40-3. - [SDR F3LA200200094](https://openairdocs.org/sdr/F3LA200200094.md): Panel · corroded · Feb 28, 2002 · N118RW · Boeing 7372Y5 · Cargo Compartments > DURING C-3 CHECK, INSPECTION REPORTED CORROSION AT SCREW HOLES ON TRANSITION PANEL AT STA 500-520. FABRICATED AND INSTALLED REPLACEMENT TRANSITION PANEL PER SRM 51-21-41. - [SDR F3LA200200093](https://openairdocs.org/sdr/F3LA200200093.md): Web · corroded · Feb 28, 2002 · N118RW · Boeing 7372Y5 · Fuselage Miscellaneous Structure > DURING C-3 CHECK, INSPECTION REPORTED CORROSION ON WEB AT STA 797 BETWEEN STR 22-R AND 24-R. REPLACED WEB PER SRM 51-30-2 AND 51-10-1. - [SDR F3LA200200092](https://openairdocs.org/sdr/F3LA200200092.md): Skin · cracked · Feb 27, 2002 · N118RW · Boeing 7372Y5 · Fuselage Main, Plate/Skin > DURING C-3 CHECK, INSPECTION REPORTED L2 DOOR CUTOUT CRACKED AT FWD LOWER CORNER OUTER SKIN APPROXIMATELY 1 INCH FROM RIVET TO DOOR CORNER. REPAIRED DAMAGE PER SRM 53-30-3. - [SDR F3LA200200091](https://openairdocs.org/sdr/F3LA200200091.md): Skin Panel · damaged · Feb 27, 2002 · N118RW · Boeing 7372Y5 · Fuselage Main, Plate/Skin > DURING C-3 CHECK, INSPECTION REPORTED MISSED DRILLED RIVET HOLE IN FWD LT. CORNER OF AFT E&E DOOR CUTOUT AT STA. 326. FABRICATED DOUBLER, TRIPLER AND FILLER PER EA 57-737-157. TREATED AND PRIMED REPAIR PARTS PER SOPM 20-41-02. INSTALLED FASTENERS PER 51-30- - [SDR F3LA200200090](https://openairdocs.org/sdr/F3LA200200090.md): Cowling · damaged · Feb 27, 2002 · N118RW · Boeing 7372Y5 · Engine Cowling System > DURING C-3 CHECK, INSPECTION REPORTED NR 1 ENGINE LT OUTBOARD COWL TOP EDGE DAMAGED BETWEEN SECOND AND LAST HINGE. REMOVED DAMAGE PER SRM 51-40-3. FABRICATED AND INSTALLED REPAIR PER SRM 51-10-2, 51-40-3 AND 51-30-2. - [SDR F3LA200200089](https://openairdocs.org/sdr/F3LA200200089.md): Mount Bracket · corroded · Feb 27, 2002 · N118RW · Boeing 7372Y5 · Drag Control Actuator > DURING C-3 CHECK, INSPECTION REPORTED LT WING REAR SPAR MOUNT TEE FOR NR 4 SPOILER OUTBOARD ACTUATOR MOUNT BRACKET CORRODED. REPLACED BRACKET AND BUSHING PER SRM 51-30-5, BOEING OHM 20-50-03 AND BOEING SOPM 20-50-01. - [SDR F3LA200200088](https://openairdocs.org/sdr/F3LA200200088.md): Beam · corroded · Feb 27, 2002 · N118RW · Boeing 7372Y5 · Fuselage Miscellaneous Structure > DURING C-3 CHECK, INSPECTION REPORTED BEAM IN FWD BULKHEAD, AFT CARGO COMPARTMENT, CORRODED AT NUT PLATE ATTACHMENT POINT FOR LOWER DUCT SHROUD BRACKETS AT LBL 20 AND WL 160. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPLACEMENT PARTS PER SRM 51-40-4. - [SDR F3LA200200087](https://openairdocs.org/sdr/F3LA200200087.md): Angle · corroded · Feb 27, 2002 · N118RW · Boeing 7372Y5 · Fuselage Miscellaneous Structure > DURING C-3 CHECK, INSPECTION REPORTED CORROSION ON AFT CARGO COMPARTMENT PANEL ATTACH ANGLE AT STA. 727, RBL 21 TO RBL 25. FABRICATED AND INSTALLED REPLACEMENT ANGLE PER SRM 51-30-2, 51-10-2 51-30-3 AND BOEING DRAWING 65-55726. - [SDR F3LA200200079](https://openairdocs.org/sdr/F3LA200200079.md): Beltframe · corroded · Feb 24, 2002 · N118RW · Boeing 7372Y5 · Fuselage Main, Frame > DURING C-3 CHECK, INSPECTION REPORTED CORROSION ON BELT FRAME AT STA 827, RBL 10. REMOVED DAMAGE, FABRICATED AND INSTALLED PER SRM 53-10-4. - [SDR F3LA200200078](https://openairdocs.org/sdr/F3LA200200078.md): Frame · cracked · Feb 24, 2002 · N118RW · Boeing 7372Y5 · Fuselage Main, Frame > DURING C-3 CHECK, INSPECTION REPORTED FRAME AT STA 82.7, RBL 10, CRACKED AT SHEAR TIE ATTACH FASTENERS IN AFT CARGO COMPARTMENT. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR PER SRM 53-10-4. - [SDR F3LA200200076](https://openairdocs.org/sdr/F3LA200200076.md): Stiffener · corroded · Feb 23, 2002 · N118RW · Boeing 7372Y5 · Fuselage Miscellaneous Structure > DURING C-3 CHECK, INSPECTION REPORTED CORROSION IN NUT PLATE HOLE AT STA 727, RBL 12, VERTICAL STIFFENER. CUT OUT DAMAGED AREA, FABRICATED REPLACEMENT PARTS AND INSTALLED PER EO 51-00-737-001 AND SRM 51-40-4. - [SDR F3LA200200075](https://openairdocs.org/sdr/F3LA200200075.md): Floorbeam · corroded · Feb 23, 2002 · N118RW · Boeing 7372Y5 · Fuselage Main, Floor Beam > DURING C-3 CHECK, INSPECTION REPORTED FLOORBEAM AT STA 967 CORRODED. FABRICATED AND INSTALLED REPLACEMENT FLOORBEAM CAP PER SRM 51-30-2. - [SDR F3LA200200074](https://openairdocs.org/sdr/F3LA200200074.md): Floor Panel · corroded · Feb 23, 2002 · N118RW · Boeing 7372Y5 · Fuselage Floor Panel > DURING C-3 CHECK, INSPECTION REPORTED CORROSION AROUND EDGES OF AFT FLOOR PANEL IN FWD CARGO COMPARTMENT. REMOVED CORROSION AROUND EDGES OF AFT FLOOR PANEL PER SRM 51-10-06. FABRICATED AND INSTALLED REPLACEMENT RETAINER STRAP PER SRM 51-10-01, 51-10-02 AND S - [SDR F3LA200200073](https://openairdocs.org/sdr/F3LA200200073.md): Strap · corroded · Feb 23, 2002 · N118RW · Boeing 7372Y5 · Fuselage Miscellaneous Structure > DURING C-3 CHECK, INSPECTION REPORTED AFT LAVATORY FLOOR WEB STRAP CORRODED AT STA 1006 TO STA 1016. FABRICATED AND INSTALLED REPLACEMENT WEB STRAP PER SRM 51-30-2. - [SDR F3LA200200071](https://openairdocs.org/sdr/F3LA200200071.md): Floor Support · corroded · Feb 23, 2002 · N118RW · Boeing 7372Y5 · Fuselage Miscellaneous Structure > DURING C-3 CHECK, INSPECTION REPORTED FLOOR SUPPORT AT STA 957, LBL 16 TO LBL 42, CORRODED. FABRICATED AND INSTALLED REPLACEMENT FLOOR SUPPORT PER SRM 53-10-2 AND 51-30-2. - [SDR F3LA200200072](https://openairdocs.org/sdr/F3LA200200072.md): Frame · corroded · Feb 23, 2002 · N118RW · Boeing 7372Y5 · Fuselage Main, Frame > DURING C-3 CHECK, INSPECTION REPORTED CORROSION ON CHORD AT STA 352, STR 28L. REPLACED DAMAGED CHORD PER SRM 51-10-2 AND SRM 51-30-2. - [SDR F3LA200200070](https://openairdocs.org/sdr/F3LA200200070.md): Panel · corroded · Feb 23, 2002 · N118RW · Boeing 7372Y5 · Fuselage Miscellaneous Structure > DURING C-3 CHECK, INSPECTION REPORTED CORROSION ON CLOSING PANEL AROUND NUT PLATES AT STA 789, RBL 39 TO RBL 46. REPLACED CLOSING PANEL PER SRM 51-10-1. - [SDR F3LA200200069](https://openairdocs.org/sdr/F3LA200200069.md): Panel · corroded · Feb 23, 2002 · N118RW · Boeing 7372Y5 · Fuselage Miscellaneous Structure > DURING C-3 CHECK, INSPECTION REPORTED CORROSION ON CLOSING PANEL AROUND NUT PLATE AT STA 789, RBL 27 TO RBL 34. REPLACED CLOSING PANEL PER SRM 51-10-1. - [SDR F3LA200200068](https://openairdocs.org/sdr/F3LA200200068.md): Floorbeam · corroded · Feb 23, 2002 · N118RW · Boeing 7372Y5 · Fuselage Main, Floor Beam > DURING C-3 CHECK, INSPECTION REPORTED TOP SURFACE OF FLOORBEAM AT STA 986 CORRODED. REPLACED FLOORBEAM CAP PER SRM 53-10-9. - [SDR F3LA200200067](https://openairdocs.org/sdr/F3LA200200067.md): Intercostal · corroded · Feb 23, 2002 · N118RW · Boeing 7372Y5 · Fuselage Miscellaneous Structure > DURING C-3 CHECK, INSPECTION REPORTED INTERCOSTAL AT STA 986 TO STA 1006, RBL 3, CORRODED. FABRICATED AND INSTALLED REPLACEMENT INTERCOSTAL PER SRM 51-30-2 AND EA 53-737-158. - [SDR F3LA200200066](https://openairdocs.org/sdr/F3LA200200066.md): Web · corroded · Feb 23, 2002 · N118RW · Boeing 7372Y5 · Fuselage Miscellaneous Structure > DURING C-3 CHECK, INSPECTION REPORTED WEB AT STA 996 TO STA 1016, RBL 40, NEXT TO R2 DOOR CORRODED. FABRICATED AND INSTALLED REPLACEMENT WEB PER SRM 51-30-2. - [SDR F3LA200200065](https://openairdocs.org/sdr/F3LA200200065.md): Strap · corroded · Feb 23, 2002 · N118RW · Boeing 7372Y5 · Fuselage Miscellaneous Structure > DURING C-3 CHECK, INSPECTION REPORTED STRAP ALONG THE BOTTOM OF PRODUCTION BREAK AT STA 1016, STR 23-L TO 23-R CORRODED. REPLACED STRAP PER SRM 51-30-2 AND BOEING DRAWING 65-46568. - [SDR F3LA200200064](https://openairdocs.org/sdr/F3LA200200064.md): Skin · cracked · Feb 23, 2002 · N118RW · Boeing 7372Y5 · Fuselage Main, Plate/Skin > DURING C-3 CHECK, INSPECTION REPORTED FUSELAGE SKIN RUBBED BY BELT 2 INCHES BELOW L-1 DOOR TOP SPIGOT (INTERIOR). PERFORMED EDDY CURRENT INSPECTION OF L-1 DOOR TOP SPIGOT INTERIOR BONDED DOUBLER AND FOUND 2 CRACKS. REPAIRED DAMAGED AREA PER EA 53-737-160. - [SDR F3LA200200063](https://openairdocs.org/sdr/F3LA200200063.md): Floorbeam · corroded · Feb 22, 2002 · N118RW · Boeing 7372Y5 · Fuselage Main, Floor Beam > DURING C-3 CHECK, INSPECTION REPORTED FLOORBEAM AT STA 986 CORRODED AT BOTTOM SURFACE AT FASTENERS THROUGH FLOORBOARDS. ALSO SHOWS EVIDENCE OF CORROSION ON TOP OF BEAM FROM BL 0 TO RBL 54 AS VIEWED FROM BELOW. REPLACED FLOORBEAM CAP AT STA 986 PER SRM 53-10- - [SDR F3LA200200062](https://openairdocs.org/sdr/F3LA200200062.md): Intercostal · corroded · Feb 22, 2002 · N118RW · Boeing 7372Y5 · Fuselage Miscellaneous Structure > DURING C-3 CHECK, INSPECTION REPORTED CORROSION ON INTERCOSTAL AT STA 847, BL 16-R. FABRICATED AND INSTALLED REPLACEMENT INTERCOSTAL PER BOEING DRAWING 65-47957, SRM 51-10-2 AND SRM 51-30-2. - [SDR F3LA200200061](https://openairdocs.org/sdr/F3LA200200061.md): Intercostal · corroded · Feb 22, 2002 · N118RW · Boeing 7372Y5 · Fuselage Miscellaneous Structure > DURING C-3 CHECK, INSPECTION REPORTED INTERCOSTAL AT STA 794, STR 27-R CORRODED. FABRICATED AND REPLACED INTERCOSTAL PER SRM 51-30-2 AND 51-20-1. - [SDR F3LA200200060](https://openairdocs.org/sdr/F3LA200200060.md): Intercostal · corroded · Feb 22, 2002 · N118RW · Boeing 7372Y5 · Fuselage Miscellaneous Structure > DURING C-3 CHECK, INSPECTION REPORTED FLOOR INTERCOSTAL IN AFT GALLEY ENTRY CORRODED STA 957, BL 16L TO BL 42L. FABRICATED AND INSTALLED REPLACEMENT FLOOR SUPPORT PER SRM 53-10-2 AND 51-30-2. - [SDR F3LA200200058](https://openairdocs.org/sdr/F3LA200200058.md): Intercostal · corroded · Feb 21, 2002 · N118RW · Boeing 7372Y5 · Fuselage Miscellaneous Structure > DURING C-3 CHECK, INSPECTION REPORTED FLOORBEAM INTERCOSTAL CORRODED FROM STA 1006 TO STA 1016, BL 0. FABRICATED AND REPLACED INTERCOSTAL PER SRM 53-10-2 AND 51-30-2. - [SDR F3LA200200057](https://openairdocs.org/sdr/F3LA200200057.md): Floorbeam · corroded · Feb 21, 2002 · N118RW · Boeing 7372Y5 · Fuselage Main, Floor Beam > DURING C-3 CHECK, INSPECTION REPORTED AFT LAVATORY TRANSVERSE BEAM CORRODED AT STA 1006 TO STA 1016, LBL 6. REPLACED TRANSVERSE FRAME PER SRM 51-30-2. - [SDR F3LA200200056](https://openairdocs.org/sdr/F3LA200200056.md): Door Frame · corroded · Feb 21, 2002 · N118RW · Boeing 7372Y5 · Fuselage Main, Structure > DURING C-3 CHECK, INSPECTION REPORTED AFT CARGO COMPARTMENT FWD DOOR FRAME AT STA 803, STR 24-R, CRACKED AND CORRODED. REPLACED AFT CARGO COMPARTMENT DOOR FRAME PER SRM 57-10-1 AND 51-30-2. - [SDR F3LA200200055](https://openairdocs.org/sdr/F3LA200200055.md): Gusset · worn · Feb 21, 2002 · N118RW · Boeing 7372Y5 · Engine Cowling System > DURING C-3 CHECK, INSPECTION REPORTED NR 1 ENGINE RT EXHAUST COWL INSIDE FLANGE ON BOTTOM OF THIRD RIB FROM FRONT WORN. REMOVED DAMAGED GUSSET FROM NR 1 ENGINE RT EXHAUST COWL. FABRICATED AND INSTALLED REPLACEMENT GUSSET PER SRM 51-21-171 AND 51-30-2. - [SDR F3LA00200054](https://openairdocs.org/sdr/F3LA00200054.md): Floorbeam · corroded · Feb 21, 2002 · N118RW · Boeing 7372Y5 · Fuselage Main, Floor Beam > DURING C-3 CHECK, INSPECTION REPORTED AFT LAVATORY TRANSVERSE FLOORBEAM CORRODED AT STA 986 TO STA 1006, LBL 10. REPLACED DAMAGED TRANSVERSE FRAME TOP CAP PER SRM 51-30-2 AND 51-10-2. - [SDR F3LA200200053](https://openairdocs.org/sdr/F3LA200200053.md): Web · corroded · Feb 21, 2002 · N118RW · Boeing 7372Y5 · Fuselage Miscellaneous Structure > DURING C-3 CHECK, INSPECTION REPORTED WEB AT STA 1016, STR 20-L, BEHIND L-2 DOOR. FABRICATED AND INSTALLED REPLACEMENT WEB PER SRM 51-30-2 AND BOEING DRAWING 65-46812. - [SDR F3LA200200052](https://openairdocs.org/sdr/F3LA200200052.md): Floorbeam · corroded · Feb 21, 2002 · N118RW · Boeing 7372Y5 · Fuselage Main, Floor Beam > DURING C-3 CHECK, INSPECTION REPORTED AFT FLOORBEAM AT STA 967 CORRODED ON TOP SURFACE. FABRICATED AND REPLACED FLOORBEAM CAP PER SRM 51-30-2. - [SDR F3LA200200051](https://openairdocs.org/sdr/F3LA200200051.md): Support · corroded · Feb 21, 2002 · N118RW · Boeing 7372Y5 · Fuselage Miscellaneous Structure > DURING C-3 CHECK, INSPECTION REPORTED AFT LAVATORY SUPPORT PARTITION FRAME CORRODED AT STA 998, 14 LBL. FABRICATED AND INSTALLED REPLACEMENT FRAME SUPPORT PER SRM 51-10-2. - [SDR F3LA200200050](https://openairdocs.org/sdr/F3LA200200050.md): Skin · corroded · Feb 21, 2002 · N118RW · Boeing 7372Y5 · Fuselage Main, Plate/Skin > DURING C-3 CHECK, INSPECTION REPORTED CORROSION ON AFT CARGO COMPARTMENT DOOR CUTOUT, LOWER FWD CORNER, AT STA 790. REPAIRED DAMAGED SECTION PER SRM 53-30-3. Next page: https://openairdocs.org/deregistered/N118RW-2004-05-11/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 = 'N118RW' AND deregistration_id = 'N118RW-2004-05-11' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N118RW-2004-05-11/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.