REF MEL 73-21-01 DMI 223505 OPERATION NOTE #4 FOR EPR INDICATION LOSS.
/PERFORMED HIGH ENERGY STOP INSPECTION PER AMM 05-51-10. BRAKE TEMP WAS 0, NO SPECIAL PROCEDURE RECOMMEND. OK FOR - [SDR UIEA2024122001179](https://openairdocs.org/sdr/UIEA2024122001179.md): Light · inoperative · Dec 20, 2024 · N718BA · Boeing 7474H6 · Emergency Lighting > UPPER DECK EMERGENCY LIGHTS INOP. MAIN DECK RH ZONE EMERGENCY LIGHTS INOP.(
R/R UPPER DECK EMERGENCY LT POWER SUPPLY IAW AMM 33-51-04 SN 49816 PN BPS7-3. TEST GOOD, ALL CHECKS PASSED. R/R PWR SUP BATTERY IAW AMM 33-51-04 SN 54269 PN 2013-1A. TEST PASSED, AL - [SDR UIEA2024040500236](https://openairdocs.org/sdr/UIEA2024040500236.md): Plate · corroded · Apr 5, 2024 · N718BA · Boeing 7474H6 · Wing Miscellaneous Structure > CORROSION- PLATE, UPPER FACE OF R/H WING T/E INBD MID FLAP TOP PNL, WBL 375(
1. PERFORM PERMANENT REPAIR - CORROSION DAMAGES ON RH WING MID FLAP UPPER SKIN PANEL WBL 375 ~ WBL 408 AREA IAW EGAT EI T2024A57M-751 REV 1 2. CONDITION CHECK IS SATISFACTORY.
) - [SDR UIEA2024040500235](https://openairdocs.org/sdr/UIEA2024040500235.md): Skin · corroded · Apr 5, 2024 · N718BA · Boeing 7474H6 · Trailing Edge Flaps > BULGE-SKIN, LOWER FACE OF RH WING T/E FORE FLAP L/E FRONT SPAR LOWER CHORD AREA, WBL 242 AND WBL 244(1. PERFORM PERMANENT REPAIR AT RH WING T/E INBD FORE FLAP LOWER SURFACE WBL 242 ~ WBL 244 IAW EGAT EI T2024A57M-752 REV 1. 2. CONDITION CHECK IS SATISFACTOR - [SDR UIEA2022101201121](https://openairdocs.org/sdr/UIEA2022101201121.md): Tire · blown · Oct 11, 2022 · N718BA · Boeing 7474H6 · Tire > LOST TIRE #8 ON TAKE-OFF OUT OF TAR (REPLACEMENT OF AXLE AND INNER/OUTER SLEEVES IN WORK) - [SDR UIEA2022030300188](https://openairdocs.org/sdr/UIEA2022030300188.md): Door Actuator · out of adjust · Mar 3, 2022 · N718BA · Boeing 7474H6 · Cargo/Baggage Doors > FOUND FWD CARGO DOOR LATCH ACTUATOR CAN NOT TURN IN LIMIT AT OPEN POSITION.(
IAW AMM TASK 52-34-00-805-005 REV 103 TO ADJUST FWD CGO DOOR LATCH ACTUATOR AT OPEN POSITION. CONDITION CHECK NORMAL AND OPERATIONAL TEST WAS SATISFIED.
) - [SDR UIEA2022030300189](https://openairdocs.org/sdr/UIEA2022030300189.md): Door Actuator · out of adjust · Mar 3, 2022 · N718BA · Boeing 7474H6 · Cargo/Baggage Doors > FOUND AFT CGO DOOR LATCH ACTUATOR CAN NOT TURN IN LIMIT AT OPEN POSITION(IAW AMM TASK 52-34-00-805-005 REV 103 TO ADJUST AFT CGO DOOR LATCH ACTUATOR AT OPEN POSITION. CONDITION CHECK NORMAL AND OPERATIONAL TEST WAS SATISFIED.
) - [SDR UIEA2022030300190](https://openairdocs.org/sdr/UIEA2022030300190.md): Door Actuator · out of adjust · Mar 3, 2022 · N718BA · Boeing 7474H6 · Cargo/Baggage Doors > FOUND FWD CGO DOOR LATCH ACTUATOR CAN NOT TURN IN LIMIT AT CLOSED POSITION(IAW AMM TASK 52-34-00-805-005 REV 103 TO ADJUST FWD CGO DOOR LATCH ACTUATOR AT CLOSED POSITION. CONDITION CHECK NORMAL AND OPERATIONAL TEST WAS SATISFIED.
) - [SDR UIEA2022030300186](https://openairdocs.org/sdr/UIEA2022030300186.md): Reservoir · inoperative · Mar 3, 2022 · N718BA · Boeing 7474H6 · Passenger/Crew Doors > FOUND L1 DOOR EMER POWER RESERVOIR LIFE LIMIT DUE(IAW AMM TASK 52-11-06-004-001 REV 103 AND AMM TASK 52-11-06-202-015 REV 103. REPLACED L1 DOOR EMERGENCY POWER RESERVOIR. JOB COMPLETED AND CONDITION CHECK NORMAL.
) - [SDR UIEA2022030300187](https://openairdocs.org/sdr/UIEA2022030300187.md): Skin · corroded · Mar 3, 2022 · N718BA · Boeing 7474H6 · Nacelle/Pylon, Bulkhead/Firewall > PITTING CORROSION - SKIN, NO. 1 PYLON AFT STRUT FAIRING FWD BULKHEAD(BLENDED OUT THE DAMAGED AREA IAW SRM 51-10-02 REV. 50. PERFORM NDT INSPECTION, REFER TO JOB CARD ATTACHING SHEET NO. 0305381. MEASURED REWORK AREA DEPTH = 0.001" LENGTH = 1", WIDTH = 0.8" - [SDR UIEA2020070201473](https://openairdocs.org/sdr/UIEA2020070201473.md): Switch · failed · Jun 30, 2020 · N718BA · Boeing 7474H6 · Landing Gear Position and Warning > FOUND SWITCH S1340 FUNCTION FAIL AT RT WLG. IAW AMM 32-36-02-004-001 / 32-36-02-A04-005 REV 98 AND WDM 32-35-12 REV 22 REPLACED SWITCH S1240. IAW AMM 32-36-02-705-001 REV 98 PERFORMED TEST OF UPLOCK MECHANISM FOR ALTERNATE EXTENSION OF THE RIGHT WING GEAR, R - [SDR UIEA2020070201475](https://openairdocs.org/sdr/UIEA2020070201475.md): Rotary Actuator · failed · Jun 30, 2020 · N718BA · Boeing 7474H6 · Landing Gear Actuator > FOUND FUNCTION FAIL AT RT WLG ALTERNATE ROTARY ACTUATOR. IAW AMM 32-36-01-004-001 REV 98 AND AMM 32-36-01-404-009 REV 98 REPLACED ROTARY ACTUATOR AT RT WLG AND PERFORMED OPERATIONAL TEST FOR ALTERNATE EXTENSION, RESULT WAS SATISFACTORY. CONDITION CHK NORMAL. - [SDR UIEA2020070201476](https://openairdocs.org/sdr/UIEA2020070201476.md): Skin · corroded · Jun 30, 2020 · N718BA · Boeing 7474H6 · Nacelle/Pylon, Plate/Skin > CORROSION - SKIN, NR 2 PYLON LT CORE COWL UPPER REAR SKIRT FAIRING ACCESS PANEL 462XJL EXTERIOR SURFACE. REMOVED DAMAGED SKIN IAW SRM 51-40-02 REV 46. INSTALL NEW SKIN IAW SRM 51-40-02, 51-40-05, AND 51-40-08, REV 46, DWG NR 311U4570 SH 1 REV A. JOB COMPLETE - [SDR UIEA2020070201477](https://openairdocs.org/sdr/UIEA2020070201477.md): Skin · deformed · Jun 30, 2020 · N718BA · Boeing 7474H6 · Fuselage Main, Plate/Skin > DEFORMATION ON FUSELAGE SKIN NEAR STA 620, S-25L TO S-26L. REPAIRED THE DEFORMATION FUSELAGE SKIN IAW EI NO T2020A53M-1669 REV 2. JOB COMPLETED AND CONDITION CHECK NORMAL. - [SDR UIEA2020070201478](https://openairdocs.org/sdr/UIEA2020070201478.md): Cargo Track · cracked · Jun 30, 2020 · N718BA · Boeing 7474H6 · Fuselage, Seat/Cargo Attach Fittings > CRACK ON THE OUTBD FLANGE OF MAIN DECK CGO RAIL 189300-31 AND WEB OF MAIN DECK CARGO FLOOR AT STA 1890, LBL 98.2. ACCOMPLISHED DAMAGE AREA REPAIR IAW EI NO T2020A53M-1664 REV 1 AND EI NO T2020A53M-1665 REV 1 AND DWG NR 814U6531 SH3 REV -. JOB COMPLETED AND C - [SDR UIEA2020070201479](https://openairdocs.org/sdr/UIEA2020070201479.md): Cargo Track · cracked · Jun 30, 2020 · N718BA · Boeing 7474H6 · Fuselage, Seat/Cargo Attach Fittings > CRACK ON THE OUTBD FLANGES OF MAIN DECK CGO RAIL (PN: 189300-27) AT STA 1790, INBD OF LBL 98.2. ACCOMPLISHED DAMAGE AREA REPAIR IAW EI NR T2020A53M-1663 REV 1. JOB COMPLETED AND CONDITION CHECK NORMAL. - [SDR UIEA2020050800951](https://openairdocs.org/sdr/UIEA2020050800951.md): Battery · discharged · May 6, 2020 · N718BA · Boeing 7474H6 · Emergency Lighting > FLIGHT DECK EMERGENCY LIGHTS INOP(
REMOVED AND REPLACED EMERGENCY LIGHT BATTERY ASSY. IAW AMM 33-51-04. EMERGENCY LIGHTS TEST PASSED, NO DEFECTS.
) - [SDR UIEA2020050800952](https://openairdocs.org/sdr/UIEA2020050800952.md): Battery · discharged · May 6, 2020 · N718BA · Boeing 7474H6 · Emergency Lighting > MAIN DECK LEFT EMERGENCY LIGHTS INOP(REMOVED AND REPLACED EMERGENCY BATTERY LIGHT ASSY IAW AMM 33-51-04. EMERGENCY LIGHT TEST PASS, NO DEFECTS.
) - [SDR UIEA2018121982865](https://openairdocs.org/sdr/UIEA2018121982865.md): Skin · cracked · Dec 19, 2018 · N718BA · Boeing 7474H6 · Fuselage Main, Plate/Skin > CRACK AND CREASE ON THE LH FUSELAGE SKIN BETWEEN STA 400 AND STA 440, S-44L.(1.ACCOMPLISH IAW EI NO.T2018A53M-7184,REV.2 2).JOB COMPLETED AND COND. CHK NML.
) - [SDR UIEA2018121982866](https://openairdocs.org/sdr/UIEA2018121982866.md): Structure · cracked · Dec 19, 2018 · N718BA · Boeing 7474H6 · Fuselage Main, Structure > DEVIATIONS AND 1 EA CRACK FASTENER HOLE FOUND DURING PERFORMING SB 747-53A2305 FOR RH SIDE.(1.ACCOMPLISH I.A.W. EI NO.T2018A53M-7178 REV.1
2.JOB COMPLETED AND COND CHK SATISFIED.
) - [SDR UIEA2018121982868](https://openairdocs.org/sdr/UIEA2018121982868.md): Tee Fitting · corroded · Dec 19, 2018 · N718BA · Boeing 7474H6 · Fuselage Main, Attach Fittings > CORROSION-TEE OF RH BODY GEAR W/W LONGERON BOX AT STA 1394.RBL.120(1.REMOVE DAMAGE PARTS I.A.W. SRM 51-40-02,REV.41.
2.FABRICATE PART I.A.W. EI NO.T2018P53M-7223,REV.0.
3.INSTALL FABRICATE PART I.A.W. SRM 51-40-02,REV.41 AND DWG NO.05B15002,ID 0 - [SDR UIEA2018121982867](https://openairdocs.org/sdr/UIEA2018121982867.md): Bracket · corroded · Dec 19, 2018 · N718BA · Boeing 7474H6 · Fuselage Main, Attach Fittings > CORROSION ON BRACKET OF RH SIDE LATERAL CENTRAL CONTROL PACKAGE.(
1.REMOVE DAMAGE PART I.A.W. SRM 51-40-02 REV.41
2.ACCOMPLISHED EI NO.T2018A53M-7267 REV.0.
3.INSTALL NEW FAB PART I.A.W. SRM 51040-02 REV.41 AND DWG NO.25141020 ID 0003 REV.K
CORROSION-FITTING,R/H WING NO.16 KRUEGAR FLAP FOLDING NOSE LINK LOWER FITTING.(
1.I.A.W. AMM 20-51-01-912-008 REV.94 REMOVED R/H WING NO.16 KRUEGAR FLAP FOLDING NOSE INBD LINK LOWER FITTING.
2.REF EI NO T2018A57M-7285 REV.0 AND JC ATTACHING SHEET NO.01 - [SDR UIEA2018121982870](https://openairdocs.org/sdr/UIEA2018121982870.md): Spar · corroded · Dec 19, 2018 · N718BA · Boeing 7474H6 · Fuselage Main, Frame > CORROSION DAMAGE ON THE REAR SPAR WEB OF CENTER WING AT STA 1241 LBL.91.(
1.REPAIR DAMAGE AREA I.A.W. EI NO.T2018A57M-7290,REV.0
2.JOB COMPLETED AND CONDITION CHECK NORMAL.
) - [SDR UIEA2018121982871](https://openairdocs.org/sdr/UIEA2018121982871.md): Plate · corroded · Dec 19, 2018 · N718BA · Boeing 7474H6 · Wing Main, Frame Structure > CORROSION-PLATE,R/H WING INBD T/E CAVITY REAR SPAR NO.3 TANK JETTISON PUMP BONDING END AREA, WS 425(1.REPAIR DAMAGE AREA I.A.W. EI NO:T2018A57M-7278,REV.0.
2.JOB COMPLETED AND CONDITION CHECK NORMAL.
) - [SDR UIEA2017070601114](https://openairdocs.org/sdr/UIEA2017070601114.md): Power Supply · no test · Jul 1, 2017 · N718BA · Boeing 7474H6 · Emergency Lighting > FOUND ALL EMERGENCY LIGHTS CANNOT STAY ON FOR A MINIMUM OF 15 MINUTES IAW AMM 33-51-04-002-009-001 AND 33-51-04-402-012-001 REV 89. REPLACED THE POWER SUPPLIESIAW AMM 33-51-04-402-012-001 REV.89. PERFORMED LIGHT TEST AND RESULT WAS SATISFACTORY. - [SDR UIEA2017070301094](https://openairdocs.org/sdr/UIEA2017070301094.md): Longeron · corroded · Jul 1, 2017 · N718BA · Boeing 7474H6 · Fuselage Main, Structure > CORROSION ON THE INBD OF RT OVERWING LONGERON BETWEEN BS 1264 AND 1279. REPAIRED THE LONGERON IAW EI T2017A53M-1446, REV 1. - [SDR UIEA2017070301096](https://openairdocs.org/sdr/UIEA2017070301096.md): Web · cracked · Jul 1, 2017 · N718BA · Boeing 7474H6 · Fuselage Miscellaneous Structure > CRACKED WEB ON MAIN DECK CARGO FLOOR NEAR BS 1790, LBL 101. REPAIRED THE DAMAGED AREA IAW T2017A53M-1407, REV 1. - [SDR UIEA2017070301097](https://openairdocs.org/sdr/UIEA2017070301097.md): Bracket · corroded · Jul 1, 2017 · N718BA · Boeing 7474H6 · Fuselage Miscellaneous Structure > CORRODED BRACKET, RT BODY MLG W/W FWD BULKHEAD TORQUE BOX SUPPORT BRACKET. REMOVED THE DAMAGED PARTS IAW SRM 51-40-02, REV 37. INSTALLED THE NEW PARTS IAW DWG 65B15210, SH8 REV J, SRM 51-40-02, REV 37, AND DWG 65B15210 SH44, REV C. - [SDR UIEA2017070301098](https://openairdocs.org/sdr/UIEA2017070301098.md): Angle · corroded · Jul 1, 2017 · N718BA · Boeing 7474H6 · Fuselage Miscellaneous Structure > CORRODED ANGLE ON THE RT SIDE OVERWING LONGERON INSTALLATION NEAR BS 1255, RBL 127.5 WL 160. FABRICATE A NEW ANGLE IAW EI T2017P53M-1452 REV.0.. REPLACED THE DAMAGED ANGLE IAW SRM 51-40-02, REV 37, AND DWG 65B15096, SHEET 3, REV H. - [SDR UIEA2017070301099](https://openairdocs.org/sdr/UIEA2017070301099.md): Web · corroded · Jul 1, 2017 · N718BA · Boeing 7474H6 · Wing Miscellaneous Structure > CORROSION DAMAGES ON THE WEB, UPPER CHORD AND UPPER STRAP OF RT WING LEADING EDGE.. REPAIRED IAW EI T2017A57M-1451 REV.1. CONDITION CHECK NORMAL.) - [SDR UIEA2017070301100](https://openairdocs.org/sdr/UIEA2017070301100.md): Skin · corroded · Jul 1, 2017 · N718BA · Boeing 7474H6 · Wing, Plate/Skin > CORROSION ON THE RT WING INTERSPAR LWR SKIN LOWER SURFACE A ROUND SURGE TANK SUMP DRAIN. ACCOMPLISHED IAW EI T2017A57M-1457 REV 1 JOB COMPLETED AND CONDITION CHECK NORMAL.. - [SDR UIEA2017070301101](https://openairdocs.org/sdr/UIEA2017070301101.md): Structure · corroded · Jul 1, 2017 · N718BA · Boeing 7474H6 · Wing Miscellaneous Structure > CORROSION CHORD OLES 1549, RT WING L/E COMPT UPPER SIDE. RMV DAMAGE DAMAGE IAW SRM 51-10-02 REV 36. WITHIN ALLOWABLE LIMIT IAW SRM 57-20-10-1A-0 REV.36 AND NDT INSP RESULT REF TO JOB CARD ATTACHING SHEET NO. 007754 3. JOB COMPLETED AND CONDITION CHECK NOR - [SDR UIEA2017070301102](https://openairdocs.org/sdr/UIEA2017070301102.md): Beam · corroded · Jul 1, 2017 · N718BA · Boeing 7474H6 · Wing Main, Frame Structure > BEAM CORRODED, OLES 1351, RT WING L/E COMPT. REMOVED DAMAGE IAW SRM 51-20-02 REV 36, FOUND WITHIN ALLOWABLE LIMITS IAW SRM 57-41-13-1A-1 REV 36. - [SDR UIEA2017070301103](https://openairdocs.org/sdr/UIEA2017070301103.md): Web · corroded · Jul 1, 2017 · N718BA · Boeing 7474H6 · Wing Miscellaneous Structure > WEB CORRODED ON RT WING L/E COMPT FWD SIDE. REMOVED DAMAGE IAW SRM 51-10-02 REV 36. FOUND WITHIN ALLOWABLE LIMITS IAW SRM 57-41-13-1A-1, REV 36. - [SDR UIEA2017070301105](https://openairdocs.org/sdr/UIEA2017070301105.md): Indicator · inoperative · Jul 1, 2017 · N718BA · Boeing 7474H6 · Attitude Gyro and Indicating System > STANDBY ATTITUDE INDICATOR INOPERATIVE. REPLACED THE STANDBY ATTITUDE INDICATOR IAW AMM 34-24-01-004-001 AND 34-24-01-404-005 REV 89. PERFORMED STBY ATT INDICATOR INSTALLATION TEST AND THE RESULT WAS SATISFACTORY IAW AMM 34-24-01-4040-005 REV 89. - [SDR UIEA2017070301106](https://openairdocs.org/sdr/UIEA2017070301106.md): Actuator · no test · Jul 1, 2017 · N718BA · Boeing 7474H6 · Landing Gear Retraction/Extension System > OPS TEST FAILED, ALTERNATE EXTENSION SYSTEM OF THE LT WING MLG. REPLACED THE LT WING MLG ALTERNATE ELECTRICAL ACTUATOR IAW AMM 32-36-01-004-001, REV 89, AND AMM 32-36-01-404-009, REV 89. CHECKED NORMAL. - [SDR UIEA2017030800310](https://openairdocs.org/sdr/UIEA2017030800310.md): Cover · cracked · Mar 8, 2017 · N718BA · Boeing 7474H6 · Rudder Control System > ON FLIGHT CONTROL CHECK PRIOR TO TAXI, EXPERIENCED STICKING, SNAPPING, INAPPROPRIATE RIGHT RUDDER RETURN. CONDITION SEEMED TO AMELIORATE WITH REPETITION BUT DID NOT CORRECT ITSELF. INITIAL INSPECTION FOUND THE RUDDER PEDAL COVER ASSEMBLY WAS CRACKED, THIS CAUS - [SDR UIEA2016020800078](https://openairdocs.org/sdr/UIEA2016020800078.md): Unknown · malfunctioned · Feb 8, 2016 · N718BA · Boeing 7474H6 · Aileron Control System > EICAS MSG, AILERON LOCKOUT ON CLIMB OUT. FOUND CMC 27322 & 27001. REPLACED RT SRM IAW AMM 27-41-02. - [SDR UIEA2016020300045](https://openairdocs.org/sdr/UIEA2016020300045.md): Skin · corroded · Feb 2, 2016 · N718BA · Boeing 7474H6 · Horizontal Stabilizer, Plate/Skin > CORROSION ON UPPER SKIN OF HORIZONTAL STABILIZER, CTR SECTION AT STRINGER 8C, LBL 9 & STRINGER 10C, LBL 3. REMOVED RIVETS FOR ACCESS IAW SRM 51-40-02-0G-0 REV 2. BLENDED OUT THE CORROSION AREA IAW SRM 51-10-02 REV 32. PERFORMED DETAIL VISUAL INSPECTION ON T - [SDR UIEA2016020600076](https://openairdocs.org/sdr/UIEA2016020600076.md): Fire Bottle · damaged · Feb 2, 2016 · N718BA · Boeing 7474H6 · Extinguishing System > FOUND MAIN DECK CARGO HALON FIRE EXTINGUISHER DAMAGE AT SWING TAIL RT, LT & TTL 2 EACH. IAW AMM 26-26-01-000-801 REV 85 & AMM 26-26-01-400-801 REV 85 REPLACED MD CARGO HALON FIRE EXTINGUISHER AT SWING TAIL RT & LT, TTL 2 EACH. JOB COMPLETED & COND CHECKED NO - [SDR UIEA2016020500054](https://openairdocs.org/sdr/UIEA2016020500054.md): Static Inverter · failed · Feb 2, 2016 · N718BA · Boeing 7474H6 · AC Inverter > FOUND MAIN STATIC INVERTER FUNCTIONAL FAILED. IAW AMM 24-29-01-004-001-001 & 24-29-01-404-005-001 REV 85, REPLACED MAIN STATIC INVERTER & COND CHECKED NORMAL. IAW AMM 24-29-01-404-005-001 REV 85 STEP D TESTED MAIN STATIC INVERTER & THE RESULT WERE SATISFACTO - [SDR UIEA2016020500049](https://openairdocs.org/sdr/UIEA2016020500049.md): Keelbeam · corroded · Feb 2, 2016 · N718BA · Boeing 7474H6 · Fuselage Main, Keel > CORROSION ON RT KEEL BEAM LOWER CHORD 65B15074-6, BETWEEN STATION 1466 & 1470, WL 86 - 91. ACCOMPLISHED EI NR T2015A53B-2813 REV 3. JOB COMPLETED & COND CHECKED NORMAL. - [SDR UIEA2016020300038](https://openairdocs.org/sdr/UIEA2016020300038.md): Door Frame · cracked · Feb 2, 2016 · N718BA · Boeing 7474H6 · Passenger/Crew Doors > FOUND CRACK ON FRAME OF L1 ENTRY DOOR, FWD UPPER CORNER. ACCOMPLISHED EI NR T2015A52B-2795 REV 2. JOB COMPLETED & COND CHECKED NORMAL. - [SDR UIEA2016020300039](https://openairdocs.org/sdr/UIEA2016020300039.md): Skin · corroded · Feb 2, 2016 · N718BA · Boeing 7474H6 · Wing, Plate/Skin > CORROSION ON THE LT WING UPPER SKIN, UPPER SURFACE AT STRINGER 2, NEAR LBBL 127.58. REMOVED FOR ACCESS REFER TO JC SHEET 0062820. BLENDED THE CORROSION AREA IAW SRM 51-10-02-0G-0 REV 32. DETAIL DATA REFER TO JC SHEET 0060187 & DATA SHEET 9050082. ACCOMPLIS - [SDR UIEA2016020300044](https://openairdocs.org/sdr/UIEA2016020300044.md): Keelbeam · corroded · Feb 2, 2016 · N718BA · Boeing 7474H6 · Fuselage Main, Keel > CORROSION DAMAGE WAS FOUND ON THE KEEL BEAM WEB, AT STATION 1276, WL 116 & LBL 9. REMOVE THE AFFECTED FASTENERS IAW SRM 51-40-02 REV 32 2. BLEND OUT THE DAMAGED AREA TO REMOVE THE CORROSION IAW SRM 51-10-02 REV 32. ACCOMPLISHED EI NO T2015A53B-2801 REV 2. - [SDR UIEA2015012600011](https://openairdocs.org/sdr/UIEA2015012600011.md): Autopilot Sys · disconnected · Jan 26, 2015 · N718BA · Boeing 7474H6 · Autopilot System > ENCOUNTERED MOUNTAIN WAVE & AIRSPEED INDICATED. ACCOMPANIED BY SIREN. AUTOPILOT DISCONNECTED & ACFT RETURNED TO NORMAL PARAMETERS. PERFORMED CONDITIONAL INSPECTION IAW AMM 05-51-03, ALL FOUND TO BE NORMAL, NO DEFECTS NOTED. - [SDR UIEA2014101000478](https://openairdocs.org/sdr/UIEA2014101000478.md): Keelbeam · corroded · Oct 10, 2014 · N718BA · Boeing 7474H6 · Fuselage Main, Keel > FIND KEEL BEAM STRUCTURE LOWER CHORD HAD CORROSION NEAR PANEL 191AL, STATION 999, LBL 9 & WL 91. REPAIRED DAMAGE AREA IAW EI NO T2014A53B 2597 SEQUENCE A & B REV 2. JOB COMPLETED & CONDITION CHECKED SATISFACTORY. - [SDR UIEA2014101000479](https://openairdocs.org/sdr/UIEA2014101000479.md): Access Panel · damaged · Oct 10, 2014 · N718BA · Boeing 7474H6 · Nacelle/Pylon, Plate/Skin > SINK SCREWS OF THE ACCESS PANEL NR 452 KR ON & NR 1 PYLON NEAR ABOVE THE EXHAUST SLEEVE. ACCOMPLISHED REPAIR IAW EI NO T2014A54B 2782 REV 1. CONDITION CHECKED NORMAL & JOB COMPLETED. Next page: https://openairdocs.org/aircraft/N718BA/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 = 'N718BA' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N718BA/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.