R/R LEFT ADC REF AIPC 34-12-01-61 & AMM 34-12-01-004-205. AIR DATA SYSTEM OPS CHECK NORMAL IAW AMM 34-12-00-715-001.
) - [SDR UIEA2026102300993](https://openairdocs.org/sdr/UIEA2026102300993.md): Fire Warning · false activation · Oct 12, 2026 · N472MC · Boeing 74745E · Fire Detection > CARGO FIRE AFT MASTER WARNING AFTER LANDING. PERFORMED LWR CARGO SMOKE DETECTION OPS TEST, TEST PASSED IAW AMM 26-16-00. - [SDR UIEA2026052900368](https://openairdocs.org/sdr/UIEA2026052900368.md): Pseu · faulted · May 29, 2026 · N472MC · Boeing 74745E · Landing Gear Door Retract Section > GEAR DOOR ADVISORY MSG AFTER TAKE OFF. GEAR DOOR & GEAR MONITOR STATUS MESSAGES. FOUND FAULTS J6 32795, 32717, 326675 & 32677. T/S PERFORMED PER FIM 32-61 TASK 885, 882, 865 & 867. WIRE RESISTANCE CHECK OK. R & R PSEU PER AMM 32-05-03, IPC 32-2426 & 32-31-61 - [SDR UIEA2025111901313](https://openairdocs.org/sdr/UIEA2025111901313.md): Duct · damaged · Nov 19, 2025 · N472MC · Boeing 74745E · Pneumatic Distribution System > BLEED 2 DUCT LEAK RH STATUS MSG. R & R R4 PDU PNEUMATIC DUCT IAW AMM 27-81-03-002-001. OPS & LEAK CHECKED OK. - [SDR UIEA2025090401155](https://openairdocs.org/sdr/UIEA2025090401155.md): Rivet · damaged · Sep 6, 2025 · N472MC · Boeing 74745E · Fuselage Structure (General) > STA 200 STR 31AL L/H 1 EA RIVET FOUND LIGHTNING STRIKE. STA 200 STR 31AL L/H 1EA RIVET HEAD LIGHTNING STRIKE REPAIRED IAW SRM 53-00-01-2R-9 REPAIR 9 SECTION II STEP 4, BLIND FASTENER REPAIR. THIS REPAIR IS CATEGORY C REPAIR. NO FURTHER DEFECTS NOTED. - [SDR UIEA2025090401156](https://openairdocs.org/sdr/UIEA2025090401156.md): Rivet · damaged · Sep 6, 2025 · N472MC · Boeing 74745E · Fuselage Structure (General) > FX - STA 200 STR 23-24A R/H 1EA RIVET FOUND LIGHTNING STRIKE. STA 200 STR 23-24A R/H 1EA RIVET HEAD LIGHTNING STRIKE REPAIRED IAW SRM 53-00-01-2R-9 REPAIR 9 SECTION II STEP 4, BLIND FASTENER REPAIR. THIS REPAIR IS CATEGORY C REPAIR. NO FURTHER DEFECTS NOTED. - [SDR UIEA2025090401157](https://openairdocs.org/sdr/UIEA2025090401157.md): Rivet · damaged · Sep 6, 2025 · N472MC · Boeing 74745E · Fuselage Structure (General) > FX - STA 215 STR 31AL L/H 1EA RIVET FOUND LIGHTNING STRIKE STA 21 STR 31AL L/H 1EA RIVET HEAD LIGHTNING STRIKE REPAIRED IAW SRM 53-00-01-2R-9 REPAIR 9 SECTION II STEP 4, BLIND FASTENER REPAIR. THIS REPAIR IS A CATEGORY C REPAIR. NO FURTHER DEFECTS NOTED - [SDR UIEA2025090401158](https://openairdocs.org/sdr/UIEA2025090401158.md): Rivet · damaged · Sep 6, 2025 · N472MC · Boeing 74745E · Fuselage Structure (General) > FX - STA 140-160 STR 24A R/H 1EA RIVET FOUND LIGHTNING STRIKE. FX - STA 140-160 STR 24A RT 1EA RIVET HEAD LIGHTNING STRIKE REPAIRED IAW SRM 53-00-01-2R-9 REPAIR 9 SECTION II STEP 4, BLIND FASTENER REPAIR. THIS REPAIR IS A CATEGORY C REPAIR. NO FURTHER DEFECTS - [SDR UIEA2025090401159](https://openairdocs.org/sdr/UIEA2025090401159.md): Rivet · damaged · Sep 6, 2025 · N472MC · Boeing 74745E · Fuselage Structure (General) > FX - STA 160 STR 24A-26 R/H 1EA RIVET FOUND LIGHTNING STRIKE(FX - STA 160 STR 24A-26 R/H 1EA RIVET HEAD LIGHTNING STRIKE REPAIRED IAW SRM 53-00-01-2R-9 REPAIR 9 SECTION II STEP 4, BLIND FASTENER REPAIR. THIS IS A CATEGORY C REPAIR. NO FURTHER DEFECTS NOTED< - [SDR UIEA2025090501162](https://openairdocs.org/sdr/UIEA2025090501162.md): Panel · torn · Sep 6, 2025 · N472MC · Boeing 74745E · Wing, Plate/Skin > LEFT WING INBD L/E UPPER (ILES550-ILES630) PANEL FOUND TORN. PERFORMED TIME LIMITED COMPOSITE REPAIR IAW EA-4457A244, PART 1, REV 0. NO FURTHER DEFECTS NOTED. - [SDR UIEA2025040700445](https://openairdocs.org/sdr/UIEA2025040700445.md): Rib · cracked · Apr 8, 2025 · N472MC · Boeing 74745E · Horizontal Stabilizer, Spar/Rib > EMP - RH HORI STAB TIP CLOSURE RIB LOWER CHORD CRACK.(
LOWER CHORD REPLACED AS PER SRM 51-10-02 & NEW LOWER CHORD HOLES TRANSFERRED AS PER SRM 51-40-05 AND NEW LOWER CHORD INSTALLED AS PER SRM 51-40-02. NO FURTHER DEFECTS NOTED.
) - [SDR UIEA2025040700446](https://openairdocs.org/sdr/UIEA2025040700446.md): Nut Plate · cracked · Apr 8, 2025 · N472MC · Boeing 74745E · Horizontal Stabilizer Miscellaneous Structure > EMP RH HORI STAB TIP CLOSURE RIB LOWER CHORD ATT NUT PLATE STRAP CRACK.(CRACK NUTPLATE STRAP FABRICATED & INSTALLED AS PER RI-55-10-17555 REV.A. NO FURTHER DEFECTS NOTED
) - [SDR UIEA2024080100765](https://openairdocs.org/sdr/UIEA2024080100765.md): Circuit Card · faulted · Jul 28, 2024 · N472MC · Boeing 74745E · Detection System > AFT CGO FIRE WARNING ON SHORT FINAL. R & R AFOLTS AFT CGO CIRCUIT CARD YLPA032 IAW AMM 26-10-01 & IPC 26-14-02-01. OPS CHECK / GND TEST PASS. NO DEFECTS NOTED. OK FOR SERVICE. - [SDR UIEA2024061300518](https://openairdocs.org/sdr/UIEA2024061300518.md): Filter · failed · Jun 13, 2024 · N472MC · Boeing 74745E · Aircraft Fuel Distribution System > DURING ENROUTE CLIMB FROM FL 300 TO FL 400, EICAS ENG 1 AND 4 FUEL FILTER MSG DISPLAYED.(REF FIM 73-00 RPLD 1 AND 4 FUEL FILTERS PER AMM 73-11-02 AND SUMP DRAIN CHECK NORMAL IAW AMM 73-11-02. DRY MOTOR LEAK TEST PER AMM 71-00-00 TEST 5.
) - [SDR UIEA2024040500265](https://openairdocs.org/sdr/UIEA2024040500265.md): Skin · corroded · Apr 3, 2024 · N472MC · Boeing 74745E · Wing, Plate/Skin > CORROSION - SKIN LEFT UNDERWING REAR SPAR OVERRIDE JETTISON PUMP AREA.(1. BLENDED OUT THE DAMAGE AREA IAW SRM 51-10-02-0G-0 REV 119 2. ACCOMPLISHED EI T2024A57M-345 REV 1 3. JOB COMPLETED AND CONDITION CHECK NORMAL.
) - [SDR UIEA2024040500264](https://openairdocs.org/sdr/UIEA2024040500264.md): Skin · corroded · Apr 3, 2024 · N472MC · Boeing 74745E · Wing, Plate/Skin > CORROSION - SKIN, LH WING INSPAR UPR SURFACE T/E AREA WS 469.82 ~ WS 478.80 REAR SPAR AREA(1. REMOVED THE AFFECTED FASTENERS IAW SRM 51-40-02-0G-0 REV 120 2. BLENDED OUT THE DAMAGE AREA IAW SRM 57-20-01-1A-A REV 120 3. PFM NDT INSP REFER TO JOB CARD ATTACHI - [SDR UIEA2024040500263](https://openairdocs.org/sdr/UIEA2024040500263.md): Beam · corroded · Apr 3, 2024 · N472MC · Boeing 74745E · Elevator Structure > CORROSION - FOUND L/H H.S.T T/E BEAM ELEV STA 257 LOWER CHORD CORROSION(
1. ACCOMPLISH EI T2024A55M-509 REV 0 2. ACCOMPLISHED EI T2024A55M-509 REV 1 3. JOB COMPLETED AND CONDITION CHECK NORMAL
) - [SDR UIEA2024040500262](https://openairdocs.org/sdr/UIEA2024040500262.md): Fairing · corroded · Apr 3, 2024 · N472MC · Boeing 74745E · Aerodynamic Fairings > CORROSION ON AFT WTB FAIRING LWR CHORD AT STA 1480. LBL 16 ~ RBL 16(1. REMOVE DAMAGE PART IAW SRM 51-40-02-OG-0 REV 120 2. FABRICATED PART IAW WORKSHEET 40232 3. INSTALLED FABRICATED PART IAW SRM 51-40-02-0G-0 REV 120 AND DWG 65B15085 SH4 REV L & 65B15085 S - [SDR UIEA2024040500261](https://openairdocs.org/sdr/UIEA2024040500261.md): Bracket · corroded · Apr 3, 2024 · N472MC · Boeing 74745E · Wing Miscellaneous Structure > CORROSION-BRACKET, LH WING T/E CAVITY HYD TUBE BLOCK - CLAMP WBL 178(
1. REMOVE DAMAGE PART IAW SRM 51-40-02-OG-0 REV 120 2. INSTALL NEW PART IAW SRM 51-40-02-0G-0 REV 120 AND DWG 65B14463 SHEET 5 REV K & SHEET 9 REV J 3. JOB COMPLETED
) - [SDR UIEA2024040500260](https://openairdocs.org/sdr/UIEA2024040500260.md): Floorbeam · none · Apr 3, 2024 · N472MC · Boeing 74745E · Standard Practices/Structures > PERFORM EO A453B457 SEC 42 UPPER DECK FLOOR BEAM REPEAT INSP FOUND FILLED DEVIATION AT STA 660 RBL 13(1. REMOVED DAMAGED PART IAW SRM 51-40-02-0G-01 REV 120 2. PERFORM EI T2024A53M-758 REV 0 SEQUENCE A 3. ACCOMPLISHED EI T2024A53M-758 REV 2 4. JOB COMPLETED - [SDR UIEA2024040500259](https://openairdocs.org/sdr/UIEA2024040500259.md): Spar · cracked · Apr 3, 2024 · N472MC · Boeing 74745E · Wing Spar > FOUND LH WING FRONT SPAR WEB CRACK NEAR FSSI 656(
1. REPAIR DAMAGED AREA IAW EI T2024A57M-424 REV 4 2. ACCOMPLISHED EI T2024A57M-424 REV 5 3. JOB COMPLETED AND CONDITION CHECK NORMAL
) - [SDR UIEA2024040500258](https://openairdocs.org/sdr/UIEA2024040500258.md): Skin · corroded · Apr 3, 2024 · N472MC · Boeing 74745E · Wing, Plate/Skin > FOUND LH WING LOWER SKIN HAVE CORROSION AT FSSI 628 ~ FSSI 660(1. REPAIR DAMAGED AREA IAW EI T2024A57M-480 REV 6 2. JOB COMPLETED AND CONDITION CHECK NORMAL
) - [SDR UIEA2024040500257](https://openairdocs.org/sdr/UIEA2024040500257.md): Skin · corroded · Apr 3, 2024 · N472MC · Boeing 74745E · Wing, Plate/Skin > CORROSION DAMAGES ON THE LH WING UPPER SKIN (P/N= 112U3102-3) UPPER SURFACE NEAR WS 323.82 (WBL 150.00), S-16 ~ S-17(1. REMOVED THE AFFECTED FASTENERS IAW SRM 51-40-02-0G-0 REV 120 2. BLENDED OUT THE DAMAGE AREA IAW SRM 57-20-01-1A-A REV 120 3. PFM NDT INS - [SDR UIEA2024040500256](https://openairdocs.org/sdr/UIEA2024040500256.md): Skin · corroded · Apr 3, 2024 · N472MC · Boeing 74745E · Wing, Plate/Skin > CORROSION DAMAGES ON THE LH WING UPPER SKIN (P/N= 112U3101-3) UPPER SURFACE NEAR WS 469.82, S-3 ~ S-4(
1. REMOVED THE AFFECTED FASTENERS IAW SRM 51-40-02-0G-0 REV 120 2. BLENDED OUT THE DAMAGE AREA IAW SRM 57-20-01-1A-A REV 120 3. PFM NDT INSP REFER TO JOB C - [SDR UIEA2024040500255](https://openairdocs.org/sdr/UIEA2024040500255.md): Skin · corroded · Apr 3, 2024 · N472MC · Boeing 74745E · Wing, Plate/Skin > CORROSION DAMAGES ON THE LH WING UPPER SKIN (P/N= 112U3101-3) UPPER SURFACE NEAR WBL 150.00, MID SPAR(
1. REMOVED THE AFFECTED FASTENERS IAW SRM 51-40-02-0G-0 REV=120 2. BLENDED OUT THE DAMAGE AREA IAW SRM 517-20-01-1A-A REV 120 3. PFM NDT INSP REFER TO JOB - [SDR UIEA2024040500254](https://openairdocs.org/sdr/UIEA2024040500254.md): Channel · cracked · Apr 3, 2024 · N472MC · Boeing 74745E · Fuselage Miscellaneous Structure > CRACK-CHANNEL, SEC 42 UPPER DECK TENSION TIE FOWARD CHANNEL AT STA 960LH(
1. ACCOMPLISHED TENSION TIE REPAIR AT LH STA 960 BETWEEN STR 10R AND 10L IAW EI T2024A53M-428, SEQUENCE A PART 3 REV 0 2. ACCOMPLISHED EI T2024A53-428 REV 1 AND EI ATTACHED TO W/O 9210 - [SDR UIEA2024040500253](https://openairdocs.org/sdr/UIEA2024040500253.md): Frame · cracked · Apr 3, 2024 · N472MC · Boeing 74745E · Fuselage Main, Frame > CRACK-FRAME, SEC 42 UPPER DECK TENSION TIE AT THE AREA OF ATTACHMENT TO FRAME 1 EA HOLE, AT STA 960 RH(
1. ACCOMPLISHED FRAME WEB REPAIR AT RH STA 960 BETWEEN STR 10R AND 10R IAW EI T2024A53M-428, SEQUENCE A PART 4 REV 0 2. ACCOMPLISHED EI T2024A53-428 REV 1 - [SDR UIEA2024040500252](https://openairdocs.org/sdr/UIEA2024040500252.md): Channel · cracked · Apr 3, 2024 · N472MC · Boeing 74745E · Fuselage Miscellaneous Structure > CRACK-CHANNEL, SEC 42 UPPER DECK TENSION TIE - FOWARD CHANNEL AT STA 900 LH(
1. ACCOMPLISHED TENSION TIE REPAIR AT LH, STA 900 BETWEEN STR 9L AND 10L IAW EI T2024A53M-428. SEQUENCE A PART 1 REV=0 2. ACCOMPLISHED EI T2024A53M-428 REV=1 3. CONDITION CHECK NOR - [SDR UIEA2024040500251](https://openairdocs.org/sdr/UIEA2024040500251.md): Channel · cracked · Apr 3, 2024 · N472MC · Boeing 74745E · Fuselage Miscellaneous Structure > CRACK-CHANNEL, SEC 42 UPPER DECK TENSION TIE - FOWARD CHANNEL AT STA 940 RH(
1. ACCOMPLISHED TENSION TIE REPAIR AT RH STA 940 BETWEEN STR 10R AND STR 10AR IAW EI T2024A53M-428. SEQUENCE A PART 3 REV=0 2. ACCOMPLISHED EI T2024A53M-428 REV=1 AND EI ATTACHED TO - [SDR UIEA2024040500250](https://openairdocs.org/sdr/UIEA2024040500250.md): Door Frame · corroded · Apr 3, 2024 · N472MC · Boeing 74745E · Fuselage Main, Structure > CRACK-VERTICAL FRAME, L2 MAIN ENTRY DOOR FWD UPPER SIDE.(
1. PERFORM EI T2024A52M-488, SEQUENCE A REV=0 2. ACCOMPLISHED EI T2024A52M-488 REV=1 3. JOB COMPLETED AND CONDITION CHECK NORMAL.
) - [SDR UIEA2024040500249](https://openairdocs.org/sdr/UIEA2024040500249.md): Door Frame · corroded · Apr 3, 2024 · N472MC · Boeing 74745E · Fuselage Main, Structure > FIND DOOR R1 AFT LOWER SIDE FRAME WEB CORROSION(1. PERFORM EI T2024A52M-491, SEQUENCE A. REV=0 2. ACCOMPLISHED EI T2024A52M-491. REV=1 3. JOB COMPLETED AND CONDITION CHECK NORMAL.
) - [SDR UIEA2024040500248](https://openairdocs.org/sdr/UIEA2024040500248.md): Frame · cracked · Apr 3, 2024 · N472MC · Boeing 74745E · Fuselage Main, Frame > CRACK-FRAME, LH INTERNAL FUSELAGE FRAME WEB AT STA 1060, WL 329(1. ACCOMPLISH EI T2024A53M-432 REV:1, SEQUENCE A PART 1: FRAME WEB SHEAR TIE REPAIR AT STA 1060 LH 2. ACCOMPLISHED EI T2024A53M-432, REV 2 AND EI ATTACHED TO WO 9213289(722) 3. JOB COMPLETED AN - [SDR UIEA2024040500247](https://openairdocs.org/sdr/UIEA2024040500247.md): Frame · cracked · Apr 3, 2024 · N472MC · Boeing 74745E · Fuselage Main, Frame > CRACK-FRAME, LH INTERNAL FUSELAGE FRAME WEB AT STA 1100, WL 329(
1. ACCOMPLISH EI T2024A53M-432 REV:1, SEQUENCE A PART 5: FRAME WEB SHEAR TIE REPAIR AT STA 1100 LH 2. ACCOMPLISHED EI T2024A53M-432, REV 2 AND EI ATTACHED TO W/O 9213289(1722) 3. JOB COMPLETED - [SDR UIEA2024040500246](https://openairdocs.org/sdr/UIEA2024040500246.md): Frame · cracked · Apr 3, 2024 · N472MC · Boeing 74745E · Fuselage Main, Frame > CRACK-FRAME, RH INTERNAL FUSELAGE FRAME WEB AT STA 1080, WL 329(
1. FRAME WEB SHEAR TIE REPAIR AT STA 1080 RH IAW EI T2024A53M-432, SEQUENCE A PART 4 REV=01 2. ACCOMPLISHED EI T2024A53M-432. REV: 2 3. JOB COMPLETED AND CONDITION CHECK NORMAL
) - [SDR UIEA2024040500245](https://openairdocs.org/sdr/UIEA2024040500245.md): Frame · cracked · Apr 3, 2024 · N472MC · Boeing 74745E · Fuselage Main, Frame > CRACK-FRAME, RH INTERNAL FUSELAGE FRAME WEB AT STA 1060, WL 329(1. FRAME WEB SHEAR TIE REPAIR AT STA 1060 RH IAW EI T2024A53M-432, SEQUENCE A PART 2 REV=01. 2. ACCOMPLISHED EI T2024A53M-432, REV=2 AND EI ATTACHED TO W/O 9213289(722) 3. JOB COMPLETED AND CON - [SDR UIEA2024040500244](https://openairdocs.org/sdr/UIEA2024040500244.md): Frame · cracked · Apr 3, 2024 · N472MC · Boeing 74745E · Fuselage Main, Frame > CRACK-FRAME, LH INTERNAL FUSELAGE FRAME WEB AT STA 1080, WL 329(
1. ACCOMPLISH EI T2024A53M-432, REV=1, SEQUENCE A PART 3, FRAME WEB SHEAR TIE REPAIR AT STA 1080 LH 2. ACCOMPLISHED EI T2024A53M-432 REV 2 AND EI ATTACHED TO W/O 9213289(722) 3. JOB COMPLETED A - [SDR UIEA2024040500243](https://openairdocs.org/sdr/UIEA2024040500243.md): Frame · cracked · Apr 3, 2024 · N472MC · Boeing 74745E · Fuselage Main, Frame > CRACK- FRAME - RH INTERNAL FUSELAGE FRAME WEB AT STA 1100, WL 329(
1. FRAME WEB SHEAR TIE REPAIR AT STA 1100 RH IAW EI T2024A53M-432, SEQUENCE A. REV=1 PART 6 2. ACCOMPLISHED EI T2024A53M-432, REV=2 AND EI ATTACHED TO W/O 9213289 (722) 3. JOB COMPLETED AND C - [SDR UIEA2024040500242](https://openairdocs.org/sdr/UIEA2024040500242.md): Frame · cracked · Apr 3, 2024 · N472MC · Boeing 74745E · Fuselage Main, Frame > FND BULK CGO BILGE FRAME CRACK AT STA 2260 RBL 53(
1. REPAIRED CRACK AREA IAW EI T2024A53M-518 REV-1, SEQUENCE B. 2. ACCOMPLISHED EI T2024A53M-518, REV=2 3. JOB COMPLETED AND CONDITION CHECK NORMAL.
) - [SDR UIEA2024040500241](https://openairdocs.org/sdr/UIEA2024040500241.md): Skin · dented · Apr 3, 2024 · N472MC · Boeing 74745E · Trailing Edge Flaps > DENT- PANEL 587LT EXTERNAL, LH OUTBD MID FLAP WBL 582(1. PERFORM REPAIR OF DENT SKIN DAMAGE AT L/H WING OUTBD MID FLAP TOP PANEL 587LT EXTERNAL SURFACE. PLEASE REFER TO THE JOB CARD ATTACHING SHEET FOR DETAILED REWORK INFORMATION. 2. CONDITION CHECK IS SATI - [SDR UIEA2024040500240](https://openairdocs.org/sdr/UIEA2024040500240.md): Skin · dented · Apr 3, 2024 · N472MC · Boeing 74745E · Trailing Edge Flaps > DENT- LH OUTBD FORE FLAP OUTBD TOP PNL EXTERNAL WBL 655(
1. PERFORM REPAIR OF DENT SKIN DAMAGE AT L/H WING OUTBD FORE FLAP TOP PANEL EXTERNAL SURFACE. PLEASE REFER TO THE JOB CARD ATTACHING SHEET FOR DETAILED REWORK INFORMATION. 2. CONDITION CHECK IS SATISFA - [SDR UIEA2024040500239](https://openairdocs.org/sdr/UIEA2024040500239.md): Skin · dented · Apr 3, 2024 · N472MC · Boeing 74745E · Trailing Edge Flaps > DENT PANEL 677IT EXTERNAL SURFACE, RH INBD MID FLAP WBL 373.33(
1. PERFORM REPAIR OF DENT SKIN DAMAGE AT R/H WING INBD MID FLAP PANEL 677IT EXTERNAL SURFACE. PLEASE REFER TO THE JOB CARD ATTACHING SHEET FOR DETAILED REWORK INFORMATION. 2. CONDITION CHECK IS - [SDR UIEA2024040500238](https://openairdocs.org/sdr/UIEA2024040500238.md): Skin · dented · Apr 3, 2024 · N472MC · Boeing 74745E · Trailing Edge Flaps > DENT- SKIN, R/H WING INBD MID FLAP PANEL 677IT EXTERNAL SURFACEWBL 374.83(
1. PERFORM REPAIR OF CHAFING SKIN DAMAGE AT R/H WING INBD MID FLAP PANEL 677IT EXTERNAL SURFACE. PLEASE REFER TO THE JOB CARD ATTACHING SHEET FOR DETAILED REWORK INFORMATION. 2. CONDI - [SDR UIEA2024040500237](https://openairdocs.org/sdr/UIEA2024040500237.md): Skin · chafed · Apr 3, 2024 · N472MC · Boeing 74745E · Ailerons > CHAFING - SKIN PNL, RH WING INBD AILERON OUTBD TE UPPER SKIN WBL 515(
1. PERFORM REPAIR OF CHAFING SKIN DAMAGE AT R/H WING INBD AILERON T/E OUTBD SIDE. PLEASE REFER TO THE JOB CARD ATTACHING SHEET FOR DETAILED REWORK INFORMATION. 2. CONDITION CHECK IS SATISF - [SDR UIEA2023091500833](https://openairdocs.org/sdr/UIEA2023091500833.md): Tire · unknown · Sep 14, 2023 · N472MC · Boeing 74745E · Tire > MLG TIRE #6 BLOWOUT DURING LANDING/TOUCHDOWN(
R/R MLG TIRE #6 & #5. ACCOMPLISHED A TIRE TREAD LOSS CONDITIONAL INSPECTION AS PER B747 AMM 05-51-34-201. APPLIED ATLAS AIR EA-4432A0086 FOR DAMAGE GEAR CLAMPS, EA-4453A0082 FOR 193BL DENT. REMOVED LH BODY GEAR S - [SDR UIEA2022102401172](https://openairdocs.org/sdr/UIEA2022102401172.md): Fairing · inflt separation · Oct 23, 2022 · N472MC · Boeing 74745E · Wing, Control Surfaces > #3 FLAP MOVABLE FAIRING DEPARTED AIRCRAFT ON LANDING RFD(
REMOVED ENTIRE FAIRING. PERFORMED CHAPTER 5 CONDITIONAL INSPECTION 1 AREA OF DAMAGE REPAIRED PER SRM SRM 51-70-06.
) - [SDR UIEA2022100601094](https://openairdocs.org/sdr/UIEA2022100601094.md): None · none · Oct 6, 2022 · N472MC · Boeing 747 · Central Warning > SLOW SPEED REJECTED TAKE OFF DUE TO SINGLE SOURCE CAUTION AURAL WARNING(REMOVED AND REPLACED LH AND RH AURAL WARNING CARD (PRINTED CIRCUT ASSY - SYNTHESIZER) AND PERFORMED AURAL WARNING SYS TEST PER AMM 31-50-00/501 AND 31-51-03/401. TEST OK.
) - [SDR UIEA2022083000927](https://openairdocs.org/sdr/UIEA2022083000927.md): None · none · Sep 29, 2022 · N472MC · Boeing 737 · Lighting System > UPPER DECK EMER LT EXIT SIGN M4717 AT STA 690 L/H EXIT DOOR INOP.(EMER LT PWR PACK ASSY M5057 REPLACED AND INSTALLATION TEST NORMAL IAW AMM 33-51-00, 33-51-04.
) - [SDR UIEA2022091200954](https://openairdocs.org/sdr/UIEA2022091200954.md): None · none · Sep 29, 2022 · N472MC · Boeing 737 · Wing Structure > LHW I/B FORE FLAP L/E FAIRING FOUND DELAMINATION (3 LOCATION) AT CTR POSITION(PERFORMED COMPOSITE HOTBOND REPAIR AS PER SRM51-70-07 PAR.5A
) - [SDR UIEA2022091200955](https://openairdocs.org/sdr/UIEA2022091200955.md): None · none · Sep 29, 2022 · N472MC · Boeing 737 · Wing Structure > LHW-L/H O/B MID FLAP L/E FOUND DELAMINATION (56" APPROX TO EDGE)(PERFORMED COMPOSITE HOTBOND REPAIR AS PER SRM51-70-07 PAR.5A
) - [SDR UIEA2022091200956](https://openairdocs.org/sdr/UIEA2022091200956.md): None · none · Sep 29, 2022 · N472MC · Boeing 737 · Wing Structure > LHW-L/H O/B MID FLAP L/E FOUND DELAMINATION (96" APPROX TO EDGE)(PERFORMED COMPOSITE HOTBOND REPAIR AS PER SRM51-70-07 PAR.5A
) Next page: https://openairdocs.org/aircraft/N472MC/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 = 'N472MC' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N472MC/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.