# Service difficulty reports: N486EV, cancelled Jan 8, 2018 A list on [N486EV, cancelled Jan 8, 2018](https://openairdocs.org/deregistered/N486EV-2018-01-08.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 5 · 234 reports - [SDR EIAA20121108093](https://openairdocs.org/sdr/EIAA20121108093.md): Light · inoperative · Nov 8, 2012 · N486EV · Boeing 747212B · Emergency Lighting > EMERGENCY LIGHT M/D BS 390 LEFT INOP. REPLACED M/D EMERGENCY LIGHT ASSY M415 BS 390 LEFT PER AMM 33-51-07 PG 201, OPS CHECK GOOD. - [SDR EIAA20120923067](https://openairdocs.org/sdr/EIAA20120923067.md): Striker · missing · Sep 23, 2012 · N486EV · Boeing 747212B · Door Warning System > SIDE CARGO DOOR WARNING LIGHT ILLUMINATED WITH P4 CAUTION LIGHT. MX PRESSURIZED A/C TO GROUND LIMIT AND UNABLE TO DUPLICATE FAULT. IN PROGRESS CHECKING INTEGRITY OF ALL SWITCH CIRCUITS AND CHECKING ADJUSTMENT PER AMM, PLANNED TO REPLACE LOWER SILL SWITCH AND - [SDR EIAA20111219259](https://openairdocs.org/sdr/EIAA20111219259.md): Engine · malfunctioned · Dec 19, 2011 · N486EV · Boeing 747212B · Engine (Turbine/Turboprop) > NR 4 ENGINE FIRE INDICATION. CREW REPORTED NR 4 ENGINE FIRE INDICATION AND BOTH FIRE BOTTLES DISCHARGED. PASSING THRU FL310 HEAD MUFFLED THUD FROM RIGHT SIDE, NO OTHER INDICATIONS. SHORTLY AFTER NR 4 ENGINE FIRE SWITCH ILLUMINATED 30 SECONDS LATER FIRE BEL - [SDR EIAA20111012238](https://openairdocs.org/sdr/EIAA20111012238.md): Cadc · failed · Oct 12, 2011 · N486EV · Boeing 747212B · Instrument Panel > FIRST OFFICER SAT GAGE, ALTIMETER, MACH IND, FLIGHT DIRECTOR & AIRSPEED INOPERATIVE WITH ALTITUDE ALERT LIGHT ON. AUTO PILOT B INOPERATIVE, TRANSPONDER NR 2 ATC FAIL, F/O FMS HAS ADC INPUT FAIL. FOUND CADC RACK CONNECTORS DB0164 B, CHD DETERIORATED AND BURNE - [SDR EIAA2011233](https://openairdocs.org/sdr/EIAA2011233.md): Warning Switch · out of adjust · Oct 2, 2011 · N486EV · Boeing 747212B · Door Warning System > SIDE CARGO DOOR OPEN LIGHT ILLUMINATED AT FL 310-8.2 DIFF PRESS, NO LOSS OF PRESSURIZATION DURING DEPRESSURIZATION AT FL 310. LIGHT EXTINGUISH AT APP 6.2 DIFF PRESS, 9,000 FT CABIN ALT. INSPECTED DOOR WARNING SYSTEM FOR MAIN SIDE CARGO DOOR PER AMM 52-71-00 - [SDR EIAA2011232](https://openairdocs.org/sdr/EIAA2011232.md): Warning Switch · dirty · Oct 2, 2011 · N486EV · Boeing 747212B · Door Warning System > AFTER LANDING - DURING TAXI TO PARKING, L5 DOOR OPEN LIGHT ILLUMINATED. CLEANED L5 DOOR WARNING SWITCH & PERFORMED ADJ/TEST PER AMM 52-71-00 SATISFACTORY. PERFORMED ACFT PRESSURIZATION PER AMM 21-31-00. L5 DOOR WARNING LIGHT NOT ILLUMINATED. - [SDR EIAA2011231](https://openairdocs.org/sdr/EIAA2011231.md): Warning Switch · malfunctioned · Oct 2, 2011 · N486EV · Boeing 747212B · Door Warning System > SIDE CARGO DOOR OPEN LIGHT ILLUMINATED AT FL 290, COMPLETED QRH PROCEDURE AND DEPRESSURIZED AIRCRAFT. LIGHT EXTINGUISHED AT APP 5.8 DIFF. PRESSURE FL 255 CABIN ALT 8200 FT. PRESSURIZATION HELD STEADY. JETTISED 26.5 LBS OF FUEL BETWEEN POXED AND 42.25N147 OE T - [SDR EIAA2011220](https://openairdocs.org/sdr/EIAA2011220.md): Battery Pack · discharged · Aug 24, 2011 · N486EV · Boeing 747212B · Emergency Lighting > THREE EACH EMERGRENCY EXIT LIGHT FAILED TO LIGHT UP IN MAIN DECK. THREE EACH EMERGENCY LIGHT BATTERY PACKS IN MAIN DECK REMOVED AND REPLACED. OPS CHECK CARRIED OUT AS PER AMM 33-51-04 AND FOUND SATISFACTORY. - [SDR EIAA2011219](https://openairdocs.org/sdr/EIAA2011219.md): Strap · cracked · Aug 24, 2011 · N486EV · Boeing 747212B · Fuselage Miscellaneous Structure > HFEC OPEN HOLE INSP ON BS 2213 BELOW S16L FOUND STRAP CRACKED. CRACKED STRAP REMOVED. NEW STRAP AND WEB FABRICATED PER BOEING DRAWINGS 65B61849 AND 65B05000 RESPECTIVELY AND INSTALLED PER SRM 51-30-02. STRAP 65B01849-25, CRACKED WEB 65B05000-70 BS 2213 BELO - [SDR EIAA2011218](https://openairdocs.org/sdr/EIAA2011218.md): Stringer · cracked · Aug 24, 2011 · N486EV · Boeing 747212B · Nacelle/Pylon, Longeron/Stringer > NR 2 PYLON (INTERIOR), PANEL CUTOUT NR 463CL AT NAC STA 180.0, I/B SRTINGER FOUND CRACKED. CRACKED STRINGER REMOVED AND REPLACED PER SRM 51-30-02. - [SDR EIAA2011217](https://openairdocs.org/sdr/EIAA2011217.md): Frame · cracked · Aug 24, 2011 · N486EV · Boeing 747212B · Fuselage Main, Frame > FRAME AT BS 260 FWD S31A-R FOUND CRACKED. MAIN FRAME WEB AT BS 260 BETWEEN S27R AND S39R REMOVED. NEW WEB FABRICATED PER BOEING DRAWING 65B07934 AND INSTALLED PER SRM 53-10-02. - [SDR EIAA2011216](https://openairdocs.org/sdr/EIAA2011216.md): Floorbeam · damaged · Aug 24, 2011 · N486EV · Boeing 747212B · Fuselage Main, Floor Beam > MAIN DECK, BS 500 TO 520, LBL 70, UPPER DECK FLOORBEAM WEB FOUND PUNCTURED AND DENTED BY LONG SCREW. CRACKED CHORD REMOVED AND REPLACED PER SRM 51-10-02. - [SDR EIAA2011215](https://openairdocs.org/sdr/EIAA2011215.md): Floorbeam · cracked · Aug 24, 2011 · N486EV · Boeing 747212B · Fuselage Main, Floor Beam > MAIN DECK, BS 380 TO 400, RBL 10, UPPER DECK FLOORBEAM WEB UPPER CHORD FOUND CRACKED. CRACKED CHORD REMOVED AND REPLACED PER SRM 51-10-02. - [SDR EIAA2011214](https://openairdocs.org/sdr/EIAA2011214.md): Frame · damaged · Aug 24, 2011 · N486EV · Boeing 747212B · Fuselage Main, Frame > MAIN DECK RT FRAME RIVET HOLE ELONGATED AT BS 2231 AT WL 195. REPAIRED IN ACCORDANCE WITH EN 059-11 APPROVED BY BOEING ODAS. - [SDR EIAA2011213](https://openairdocs.org/sdr/EIAA2011213.md): Frame · cracked · Aug 24, 2011 · N486EV · Boeing 747212B · Fuselage Main, Frame > MAIN DECK FRAME INNER CHORD CRACKED AT BS 2231 BETWEEN S16R & S18R. REPAIRED PER B747 SRM 53-10-04, FIGURE 140. - [SDR EIAA2011212](https://openairdocs.org/sdr/EIAA2011212.md): Frame · damaged · Aug 24, 2011 · N486EV · Boeing 747212B · Fuselage Main, Frame > FRAME FOUND DAMAGED WITH DRILL HOLES AT BS 180 BETWEEN S19R & S24R. DAMAGED FRAME REMOVED AND NEW FRAME INSTALLED PER SASCO EN 068-11 APPROVED BY BOEING ODAS. - [SDR EIAA2011211](https://openairdocs.org/sdr/EIAA2011211.md): Frame · damaged · Aug 24, 2011 · N486EV · Boeing 747212B · Fuselage Main, Frame > FRAME FOUND DAMAGED WITH DRILL HOLES AT BS 180 BETWEEN S19L & S24L. DAMAGED FRAME REMOVED AND NEW FRAME INSTALLED PER SASCO EN 068-11 APPROVED BY BOEING ODAS. - [SDR EIAA2011210](https://openairdocs.org/sdr/EIAA2011210.md): Frame · damaged · Aug 24, 2011 · N486EV · Boeing 747212B · Fuselage Main, Frame > FRAME FOUND DAMAGED WITH DRILL HOLES AT BS 220 BETWEEN S22R & S23R. DAMAGED FRAME REMOVED AND NEW FRAME INSTALLED PER EN 068-11 APPROVED BY BOEING ODAS. - [SDR EIAA2011209](https://openairdocs.org/sdr/EIAA2011209.md): Frame · damaged · Aug 24, 2011 · N486EV · Boeing 747212B · Fuselage Main, Frame > FRAME FOUND DAMAGED WITH DRILL HOLES AT BS 220 BETWEEN S19L & S24L. DAMAGED FRAME REMOVED AND NEW FRAME INSTALLED PER EN 068-11 APPROVED BY BOEING ODAS. - [SDR EIAA2011208](https://openairdocs.org/sdr/EIAA2011208.md): Skin · chafed · Aug 24, 2011 · N486EV · Boeing 747212B · Nacelle/Pylon, Plate/Skin > NR 2 PYLON LOWER SPAR WEB (EXTERIOR) SY NAC STA 180 TO 250 FOUND LT & RT PLATES CHAFED ADJ TO ENGINE THRUST UPPER LINK. REPAIRED PER B747 SRM 54-30-03 FIGURE 23. - [SDR EIAA2011207](https://openairdocs.org/sdr/EIAA2011207.md): Cap · cracked · Aug 24, 2011 · N486EV · Boeing 747212B · Nacelle/Pylon Miscellaneous Structure > NR 4 PYLON STA 280 LOWER END CAP ASSY FOUND CRACKED. CRACKED LOWER END CAP ASSY REMOVED. NEW END CAP FABRICATED PER BOEING DRAWING 69B90354 AND ISTALLED PER B747 SRM 51-30-02. - [SDR EIAA2011206](https://openairdocs.org/sdr/EIAA2011206.md): Stringer · cracked · Aug 24, 2011 · N486EV · Boeing 747212B · Fuselage Main, Longeron/Stringer > REMOVE AND REPLACE REPAIR ON S37R BETWEEN BS 421 & 430. EXISTING REPAIR REMOVED AND NEW REPAIR INSTALLED PER B747 SRM 53-10-03 FIGURE 3. - [SDR EIAA2011205](https://openairdocs.org/sdr/EIAA2011205.md): Bear Strap · corroded · Aug 24, 2011 · N486EV · Boeing 747212B · Fuselage Main, Plate/Skin > L5 DOOR CUTOUT BEAR STRAP AT STA 2284 BETWEEN S24L & S25L FOUND CORRODED. REPAIRED IN ACCORDANCE WITH EN 044-11 APPROVED BY BOEING ODAS. - [SDR EIAA2011204](https://openairdocs.org/sdr/EIAA2011204.md): Stringer · cracked · Aug 24, 2011 · N486EV · Boeing 747212B · Fuselage Main, Longeron/Stringer > REMOVE AND REPLACE REPAIR ON S38L BETWEEN BS 480 TO 500. EXISTING REPAIR REMOVED AND NEW REPAIR INSTALLED PER B747 SRM 53-10-03 FIGURE 3. - [SDR EIAA2011203](https://openairdocs.org/sdr/EIAA2011203.md): Stringer · cracked · Aug 24, 2011 · N486EV · Boeing 747212B · Fuselage Main, Longeron/Stringer > REMOVE AND REPLACE REPAIR ON S37L BETWEEN BS 460 & 480. EXISTING REPAIR REMOVED AND NEW REPAIR INSTALLED PER B747 SRM 53-10-03 FIGURE 3. - [SDR EIAA2011199](https://openairdocs.org/sdr/EIAA2011199.md): Skin · cracked · Aug 24, 2011 · N486EV · Boeing 747212B · Passenger/Crew Doors > HFEC INSPECTION FOUND APPROX 1 INCH CRACK THROUGH STOP DRILLED HOLE ON L1 DOOR SKIN UPPER HINGE CUTOUT RADIUS. REPAIRED IN ACCORDANCE WITH EN 048-11 APPROVED BY BOEING ODAS. - [SDR EIAA2011163](https://openairdocs.org/sdr/EIAA2011163.md): Channel · damaged · Aug 24, 2011 · N486EV · Boeing 747212B · Fuselage Miscellaneous Structure > CHANNEL ON MAIN DECK FRAM AT BS 2020 BETWEEN S20R AND S22R DAMAGED. DAMAGED CHANNEL REMOVED. NEW CHANNEL FABRICATED AND INSTALLED PER B747 SRM 51-30-02. - [SDR EIAA2011159](https://openairdocs.org/sdr/EIAA2011159.md): Frame · damaged · Aug 24, 2011 · N486EV · Boeing 747212B · Fuselage Main, Frame > MAIN DECK FRAME DAMAGED DUE TO DRILL HOLE AT BS 1200 BETWEEN STRINGER 17R AND 21R. FRAME REPAIRED PER B747 SRM 51-4-04, FIGURE 3. - [SDR EIAA2011202](https://openairdocs.org/sdr/EIAA2011202.md): Stringer · cracked · Aug 23, 2011 · N486EV · Boeing 747212B · Fuselage Main, Longeron/Stringer > STRINGER CRACKED AT BS 220 S0. CRACKED STRINGER REMOVED AND REPLACED WITH NEW STRINGER PER B747 SRM 51-30-02. - [SDR EIAA2011201](https://openairdocs.org/sdr/EIAA2011201.md): Splice · cracked · Aug 23, 2011 · N486EV · Boeing 747212B · Fuselage Miscellaneous Structure > ZEE SPLICE FOUND CRACKED AT BS 220 S4L. NEW ZEE SPLICE FABRICATED PER BOEING DRAWING 65B07618 AND INSTALLED PER SRM 51-30-02. - [SDR EIAA2011183](https://openairdocs.org/sdr/EIAA2011183.md): Support Beam · cracked · Aug 21, 2011 · N486EV · Boeing 747212B · Wing Miscellaneous Structure > RT WING REAR SPAR CAVITY SPOILER SUPPORT BEAM UPPER CHORD AT WBL 235.2 FOUND CRACKED. CRACKED CHORD TRIMMED. HFEC INSP TO VERIFY CHORD IS CRACK FREE. FABRICATED REPAIR ANGLES AND CHORD SEGMENT AND INSTALLED PER BOEING DRAWING 65B07738-58 AND EN 049-11. - [SDR EIAA2011179](https://openairdocs.org/sdr/EIAA2011179.md): Skin · punctured · Aug 21, 2011 · N486EV · Boeing 747212B · Fuselage Main, Plate/Skin > EMP - FUSELAGE LT AT APPROX BS 2670 ADJACENT TO VERT STAB SEAL RETAINER SKIN HAS A PUNCTURE. REPAIRED PER B747 SRM 53-30-03 FIGURE 2. - [SDR EIAA2011178](https://openairdocs.org/sdr/EIAA2011178.md): Bear Strap · cracked · Aug 20, 2011 · N486EV · Boeing 747212B · Fuselage Main, Plate/Skin > HFEC INSPECTION FOUND CRACKS AT BEARSTRAP AT L3 DOOR CUTOUT EDGE AFT UPPER CORNER. REPAIRED PER B747 SRM 53-30-03 AND EN 065-11. - [SDR EIAA2011175](https://openairdocs.org/sdr/EIAA2011175.md): Spar · cracked · Aug 20, 2011 · N486EV · Boeing 747212B · Nacelle/Pylon, Frame/Spar/Rib > DURING HFEC OPEN HOLE INSPECTION ON NR 3 PYLON FRONT SPAR CHORD FOUND 2 EA HOLE CRACKED. NR 3 PYLON FRONT SPAR CHORD REPAIRED PER BOEING SB 747-54A2158 AND SASCO EN 042-11. - [SDR EIAA2011174](https://openairdocs.org/sdr/EIAA2011174.md): Bulkhead · cracked · Aug 20, 2011 · N486EV · Boeing 747212B · Fuselage Main, Bulkhead > DURING HFEC OPEN HOLE INSPECTION FOUND CRACK AT LT BS 2598 BULKHEAD INNER CHORD. REPAIRED PER SASCO EN 047-11 APPROVED BY BOEING ODAR. - [SDR EIAA2011172](https://openairdocs.org/sdr/EIAA2011172.md): Bulkhead · cracked · Aug 20, 2011 · N486EV · Boeing 747212B · Fuselage Main, Bulkhead > DURING HFEC OPEN HOLE INSPECTION FOUND CARCK AT RT BS 2598 BULKHEAD INNER CHORD. REPAIRED PER EN 052-11 APPROVED BY BOEING ODAR. - [SDR EIAA2011171](https://openairdocs.org/sdr/EIAA2011171.md): Spar · cracked · Aug 20, 2011 · N486EV · Boeing 747212B · Nacelle/Pylon, Frame/Spar/Rib > DURING HFEC OPEN HOLE INSPECTION ON NR 2 PYLON FRONT SPAR CHORD FOUND 2 HOLE CRACKS. NR 2 PYLON FRONT SPAR CHORD REPAIRED PER BOEING SB 747-54A2158 AND EN 041-11. - [SDR EIAA2011166](https://openairdocs.org/sdr/EIAA2011166.md): Doubler · cracked · Aug 19, 2011 · N486EV · Boeing 747212B · Fuselage Main, Structure > HFEC INSPECTION FOUND CRACK ON WEB DOUBLER ON L1 DOOR CUTOUT FRAME ST STA 488 FWD SIDE OF DOUBLER AT LWR EDGE OF DOOR STOP NR 1. DAMAGED FRAME REMOVED. NEW WEB DOUBLER FABRICATED PER DRAWING 65B01838-11 AND INSTALLED PER B747SRM 51-30-02. - [SDR EIAA2011164](https://openairdocs.org/sdr/EIAA2011164.md): Floorbeam · cracked · Aug 19, 2011 · N486EV · Boeing 747212B · Fuselage Main, Floor Beam > UPPER DECK FLOORBEAM WEB AT BS 330 RBL 60 FOUND CRACKED. DAMAGED WEB REMOVED. FLOORBEAM UPPER CHORD TRIMMED OUT PER SRM 51-10-01 AND REPAIRED CARRIED OUT PER BOEING DRAWING 65B28068, REV B SHEET 3 AND SB 747-53-2272, FIG 16 NOTE 3. - [SDR EIAA2011162](https://openairdocs.org/sdr/EIAA2011162.md): Strap · cracked · Aug 19, 2011 · N486EV · Boeing 747212B · Fuselage Miscellaneous Structure > OPEN HOLE HFEC INSP FOUND STRAP CRACKED AT UPPER DECK FLOORBEAM BS 340 LT COMMON TO CRES STRAPS INSTALLED ON UPPER CHORD VERTICAL FLANGE AREA. DAMAGED STRAP REMOVED. NEW STRAP FABRICATED FOR DRAWING 65B10927 AND INSTALLED FER B747 SRM 51-30-02. - [SDR EIAA2011161](https://openairdocs.org/sdr/EIAA2011161.md): Shear Tie · cracked · Aug 19, 2011 · N486EV · Boeing 747212B · Fuselage Internal Mounting Structure > MAIN DECK SHEAR TIE CRACKED AT BS 1180 AROUND LT S23 AREA. REPLACE CRACKED SHEAR TIE PER B747 SRM 51-30-02. - [SDR EIAA2011160](https://openairdocs.org/sdr/EIAA2011160.md): Floorbeam · damaged · Aug 19, 2011 · N486EV · Boeing 747212B · Fuselage Main, Floor Beam > FWD CARGO COMPARTMENT FLOORBEAM WEB AT BS 720 AT LBL 12 HAS A 1 INCH HOLE. FLOORBEAM WEB REPAIRED BER B747 SRM 53-10-04, FIG 70. - [SDR EIAA2011157](https://openairdocs.org/sdr/EIAA2011157.md): Skin · cracked · Aug 16, 2011 · N486EV · Boeing 747212B · Fuselage Main, Plate/Skin > HFEC OPEN HOLE INSPECTION FOUND CRACK ON FUSELAGE SKIN AT BS 980 S38R. FUSELAGE SKIN REPAIRED FOR B747 SRM 53-30-03, FIGURE 60 WITH MINOR DEVIATIONS APPROVED BY BOEING. - [SDR EIAA2011145](https://openairdocs.org/sdr/EIAA2011145.md): Doubler · cracked · Aug 12, 2011 · N486EV · Boeing 747212B · Service Doors > R1 MED FWD FRAME UNDER UPPER HINGE CUTOUT DOUBLER CRACKED. CRACKED DOUBLER REMOVED AND REPAIR CARRIED OUT PER B747 SRM 52-10-02, FIG 13. - [SDR EIAA2011144](https://openairdocs.org/sdr/EIAA2011144.md): Doubler · corroded · Aug 12, 2011 · N486EV · Boeing 747212B · Fuselage Miscellaneous Structure > RT BLG WW NEAR STA 1460 O/B FRAME, CEILING SKIN FOUND CORRODED. CORROSION REMOVED AND AREA BLENDED. AREA CLEANED & INSPECTED TO ENSURE COMPLETE CORROSION REMOVAL AND REPAIRED PER EN 071-11 (BOEING ODAR APPROVED REPAIR). - [SDR EIAA2011140](https://openairdocs.org/sdr/EIAA2011140.md): Stringer · damaged · Aug 12, 2011 · N486EV · Boeing 747212B · Fuselage Main, Longeron/Stringer > IN MAIN EQUIPMENT CENTER (MEC) STRINGER 36L FOUND DEFORMED AND RIVIT HOLE CRACKED AT BS 420. EXISTING REPAIR REMOVED, NEW CHORD FABRICATED PER DRAWING 65B09014, FOI CARRIED OUT OER BAC 5423 AND NEW CHORD INSTALLED PER B747 SRM 51-30-02. - [SDR EIAA2011138](https://openairdocs.org/sdr/EIAA2011138.md): Frame · corroded · Aug 12, 2011 · N486EV · Boeing 747212B · Fuselage Main, Frame > LEFT BLG WW OVERWING LONGERON AT STA 1438, FRAME STRUCTURE HAS CORROSION. EXISTING REPAIR REMOVED, NEW CHORD FABRICATED PER DRAWING 65B09014, FOI CARRIED OUT OER BAC 5423 AND NEW CHORD INSTALLED PER B747 SRM 51-30-02. - [SDR EIAA2011137](https://openairdocs.org/sdr/EIAA2011137.md): Stringer · cracked · Aug 12, 2011 · N486EV · Boeing 747212B · Fuselage Main, Longeron/Stringer > OPEN HOLE HFEC INSPECTION FOUND 2 EACH CRACKS AT FASTENER HOLES ON STRINGER 38R AT BS 980. EXISTING REPAIR REMOVED, NEW CHORD FABRICATED PER DRAWING 65B09014, FOI CARRIED OUT OER BAC 5423 AND NEW CHORD INSTALLED PER B747SRM 51-30-02, - [SDR EIAA2011135](https://openairdocs.org/sdr/EIAA2011135.md): Stringer · dented · Aug 12, 2011 · N486EV · Boeing 747212B · Fuselage Main, Longeron/Stringer > IN MAIN EQUIPMENT CENTER (MEC) STRINGER 38L BETWEEN BD 380 TO 400 FOUND DENTED. EXISTING REPAIR REMOVED, NEW CHORD FABRICATED PER DRAWING 65B09014, FOI CARRIED OUT OER BAC 5423 AND NEW CHORD INSTALLED PER B747SRM 51-30-02, - [SDR EIAA2011126](https://openairdocs.org/sdr/EIAA2011126.md): Frame · deformed · Aug 11, 2011 · N486EV · Boeing 747212B · Fuselage Main, Frame > MID FRAME DEFORMED & CHAFED AT BS 1849 AROUND RT S11 AREA. DEFORMED FRAME AT BS 1840 AT S-11R REPAIRED PER BOEING 747 SRM 51-40-03 FIG 2, DETAIL III. Next page: https://openairdocs.org/deregistered/N486EV-2018-01-08/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 = 'N486EV' AND deregistration_id = 'N486EV-2018-01-08' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N486EV-2018-01-08/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.