TWO HOLES WITH CORROSION AT HORIZONTAL STABILIZER PIVOT FITTING RH UPPER ATTACHMENTS, WERE REPAIRED I.A.W. TRE6755081 ISSUED DATE 03MAR25 & CMA-TL - [SDR UIEA2025031900343](https://openairdocs.org/sdr/UIEA2025031900343.md): Skin · punctured · Mar 15, 2025 · N1373A · Boeing 76731K · Spoilers > PUNCTURE DAMAGE TO UPPER SPOILER SKIN 6, REPAIR AS REQUIRED.(
UPPER SPOILER SKIN 6 WAS REPAIRED I.A.W B767 SRM 57-70-01-2R-1 AND SRM 51-70-04-0G-0 PAR 5 B AND 51-70-17-0G-0 PAR 4 B FIG 24 REV 127 15DEC24. NO FURTHER DEFECTS NOTED.
) - [SDR UIEA2025031900342](https://openairdocs.org/sdr/UIEA2025031900342.md): Support · corroded · Mar 15, 2025 · N1373A · Boeing 76731K · Leading Edge Devices > LH WING INBOARD FLAP TRACK #3 SUPPORT AFT ATTACHMENT HOLES, BORE WITH CORROSION (4EA).(LH WING INBOARD FLAP TRACK #3 SUPPORT AFT ATTACHMENT HOLES WERE REPAIRED I.A.W. TRE6757277 ISSUED DATE 04/ MAR/25 & CMA-TLS-25-0017. APPROVAL BY FAA FORM 8100-9 (2-02) IS - [SDR UIEA2025031900341](https://openairdocs.org/sdr/UIEA2025031900341.md): Fitting · corroded · Mar 15, 2025 · N1373A · Boeing 76731K · Horizontal Stabilizer Structure > HORIZONTAL STABILIZER PIVOT FITTING RH LOWER ATTACHMENTS, HOLE WITH CORROSION. SEE NDT INSPECTION REPORT.(
HOLE WITH CORROSION AT HORIZONTAL STABILIZER PIVOT FITTING RH LOWER ATTACHMENTS WAS REPAIRED IAW TRE6755081 ISSUED DATE 03MAR25 FAA FORM 8100-9 (2-02) - [SDR UIEA2025031900340](https://openairdocs.org/sdr/UIEA2025031900340.md): Packing · leaking · Mar 15, 2025 · N1373A · Boeing 76731K · Hydraulic System, Main > RH WING, PDU SLATS, HYDRAULIC MOTOR WITH EVIDENCE OF HYD LEAK.(
RH WING PDU HYD MOTOR PACKING WAS REPLACED AND LINES WERE TIGHTEN I.A.W AMM 27-81-11-424-029 REV. 144 22/DEC/24 TORQUE WAS APPLIED 170 LB/IN, 500 LB/IN AND 270 LB/IN, TORQUE DA TA S/N: 052412188 - [SDR UIEA2025031900339](https://openairdocs.org/sdr/UIEA2025031900339.md): Bushing · corroded · Mar 15, 2025 · N1373A · Boeing 76731K · Horizontal Stabilizer Structure > HORIZONTAL STAB, RH PIVOT PIN, SLEEVE WITH CORROSION.(
HORIZONTAL STAB RH PIVOT PIN SLEEVE WAS REPLACED WITH NR00439 IAW SRM 51-10-02-0G-0 REV 127 DATE 15 DEC 24. NO FURTHER DEFECTS NOTED.
) - [SDR UIEA2025031900338](https://openairdocs.org/sdr/UIEA2025031900338.md): Longeron · corroded · Mar 15, 2025 · N1373A · Boeing 76731K · Fuselage Miscellaneous Structure > AFT CARGO COMPARTMENT, BTW STA 1065 AND 1087, STRG 23L AND 24L, LONGERON WITH CORROSION, L=4" W=1.580".(AFT CARGO COMPARTMENT, BTW STA 1065 AND 1087, STRG 23L AND 24L, LONG ERON WITH CORROSION LEVEL 2 WAS REPLA CED IAW SRM 51-10-02-0G-0 PAR 9 REV 127 15 DEC - [SDR UIEA2025031900337](https://openairdocs.org/sdr/UIEA2025031900337.md): Support · corroded · Mar 15, 2025 · N1373A · Boeing 76731K · Trailing Edge Flaps > RIGHT WING TRAILING EDGE OUTBOARD FLAP SUPPORT #7, SUPPORT ACTUATOR HOLE WITH CRACK INDICATION AT 6 O´CLOCK APPROX.(
RIGHT WING TRAILING EDGE OUTBOARD FLAP SUPPORT #7, SUPPORT ACTUATOR HOLE WAS REPAIRED IAW TRE6757276 ISSUED DATE 21/FEB/25 & CMA-TLS-25-0006 - [SDR UIEA2025031940336](https://openairdocs.org/sdr/UIEA2025031940336.md): Support · corroded · Mar 15, 2025 · N1373A · Boeing 76731K · Trailing Edge Flaps > RIGHT WING TRAILING EDGE OUTBOARD FLAP SUPPORT #8, SUPPORT ACTUATOR HOLE WITH CORROSION INDICATION.(
RIGHT WING TRAILING EDGE OUT BOARD FLAP SUPPORT #8, SUPPORT ACTUATOR HOLE WITH CORROSION LEVEL 2 WAS REPAIRED IAW TRE6757275 ISSUED DATE FEBRUARY 21, 2025. F - [SDR UIEA2025031200280](https://openairdocs.org/sdr/UIEA2025031200280.md): Skin · damaged · Mar 15, 2025 · N1373A · Boeing 76731K · Leading Edge Devices > DURING THE REMOVAL OF SLAT #6 FOR REPAIR (NR 00005), HIDDEN DAMAGE WAS FOUND ON LH WING FIXED LEADING EDGE AT RIB LES 351.10, WITH EXCESSIVE WEAR AND HOLE.(
ON LH WING FIXED LEADING EDGE AT RIB LES 351.10, DAMAGE WAS REPAIRED I. A.W. SRM 57-41-09-2R-2 FIGURE - [SDR UIEA2025031200279](https://openairdocs.org/sdr/UIEA2025031200279.md): Case · corroded · Mar 15, 2025 · N1373A · Boeing 76731K · Turbine Engine Air Inlet Section > ENG 2, FAN CASE, AT 6' O CLOCK, UNDER STRUT AREA, BASE WITH CORROSION L=2.100" W=1"(
ENG 2, FAN CASE, AT 6' O CLOCK, UNDER STRUT AREA, BASE, CORROSION LEVEL 1 WAS REWORKED, EVALUATED, INSPECTED AND FOUND TO BE WITHIN ALLOWABLE LIMITS IAW AMM 72-33-00-206-001 - [SDR UIEA2025031200278](https://openairdocs.org/sdr/UIEA2025031200278.md): Case · corroded · Mar 15, 2025 · N1373A · Boeing 76731K · Turbine Engine Air Inlet Section > ENG 1, AFT FAN CASE, AT 5 TO 6 O'CLOCK APROX, WITH SEVERAL POINTS OF CORROSION (3EA).(
ENG 1, AFT FAN CASE, AT 5 TO 6 O'CLOCK APROX, CORROSIONS LEVEL 1 WAS REWORKED, EVALUATED, INSPECTED AND FOUND TO BE WITHIN ALLOWABLE LIMITS. NO FURTHER DEFECTS NOTED.
) - [SDR UIEA2025031900255](https://openairdocs.org/sdr/UIEA2025031900255.md): Skin · dented · Mar 15, 2025 · N1373A · Boeing 76731K · Trailing Edge Flaps > LH WING INBOARD TRAILING EDGE FLAP, LOWER AREA UPPER SKIN WITH SEVERAL DENTS.(ONE DENT WAS REPAIRED IAW SRM 57-53-01-2R-1 PAG.1-7 FIG. 201 SHEET 4 AND SRM 51-70-10-2R-4 REPAIR 4
/FIG.201 SHEET 1 PAG.1-22 AND THREE FOUND WITHIN LIMITS IAW B767 SRM 57 - [SDR UIEA2025031900254](https://openairdocs.org/sdr/UIEA2025031900254.md): Skin · punctured · Mar 15, 2025 · N1373A · Boeing 76731K · Elevator, Plate/Skin > RH OUTBOARD ELEVATOR, LOWER AND UPPER SKIN WITH A PUNCTURE BTW ELEV STA 200 AND 176, AT 2" FROM TRAILING EDGE.(
RH OUTBOARD ELEVATOR, LOWER AND UPPER SKIN WAS REPAIRED IAW SRM 55-20-01-2R-1 FIG.201 SHEET 2 PAG.2-3 AND SRM 51-70-04-0G-0 PAR.5.D FIG.6 PAG.17,3 - [SDR UIEA2025031900253](https://openairdocs.org/sdr/UIEA2025031900253.md): Beam · corroded · Mar 15, 2025 · N1373A · Boeing 76731K · Cargo/Baggage Doors > AFT CARGO DOOR, BEAM INNER CHORD, BTW STA 1285 AND STA 1329 STRG 23 WITH CORROSION AROUND FASTENER HOLES (L= 1.250" W=1 ").(
REPAIRED IN ACCORDANCE WITH TRE6752056 (BOEING COMMUNICATION MESSAGE CMA-TLS-25-0012). NO FURTHER DEFECTS NOTED
) - [SDR UIEA2025031000252](https://openairdocs.org/sdr/UIEA2025031000252.md): Skin · dented · Mar 15, 2025 · N1373A · Boeing 76731K · Leading Edge Devices > LEFT WING, SLAT 6 INBOARD FACE WITH DENT APRX 10€Œ OF OUTBOARD EDGE.(LEFT WING, SLAT 6 INBOARD FACE WITH DENT APRX 10€Œ OF OUTBOARD EDGE WAS REPAIRED IAW SRM 57-43-02-2R-1 FIG.201 PAG.2-3 AND SRM 51-70-10-2R-4 REPAIR 4 FIG.202 SHEET 1 PAG.1,8,16. NO FURTH - [SDR UIEA2025031000251](https://openairdocs.org/sdr/UIEA2025031000251.md): Support · corroded · Mar 15, 2025 · N1373A · Boeing 76731K · Wing Main, Frame Structure > RIGHT WING TRAILING EDGE INBOARD FLAP #5 SUPPORT MECHANISM 6-6 OUTER PIN WITH SEVERAL CORROSION IN THE INNER BORE.(
RIGHT WING TRAILING EDGE INBOARD FLAP #5 SUPPORT MECHANISM 6-6 OUTER PIN WAS REPLACED IAW AMM TASK 27-51-04-402-135 REV 144. NO FUTHER DEFECTS - [SDR UIEA2025031900250](https://openairdocs.org/sdr/UIEA2025031900250.md): Skin · corroded · Mar 15, 2025 · N1373A · Boeing 76731K · Horizontal Stabilizer, Plate/Skin > CORROSION ON THE UPPER SKIN OF THE HORIZONTAL STABILIZER CENTER SECTION, RH SIDE.(
THE UPPER SKIN OF THE HORIZONTAL STABILIZER CENTER SECTION, RH SIDE MWAS REWORKED, BLEND OUT AND INSPECTIONS PER MXA EO NO. TRE6755080 (BOEING COMMUNICATION MESSAGE CMA-TLS-25 - [SDR UIEA2025031900247](https://openairdocs.org/sdr/UIEA2025031900247.md): Skin · dented · Mar 15, 2025 · N1373A · Boeing 76731K · Leading Edge Devices > SLAT #5, LEADING EDGE EXTERNAL SKIN, LOWER INBOARD EDGE WITH A DENT.(
SLAT #5, LEADING EDGE EXTERNAL SKIN, LOWER INBOARD EDGE DAMAGE WAS REPAIRED IAW. TRE6757274 ISSUED DATE 14FEB25 & CMA-TLS-25-0003 DATE 25FEB25. NO FURTHER DEFECTS NOTED
) - [SDR UIEA2025031900246](https://openairdocs.org/sdr/UIEA2025031900246.md): Skin · corroded · Mar 15, 2025 · N1373A · Boeing 76731K · Fuselage Main, Plate/Skin > FUSELAGE SECTION 48, APU INTAKE DOOR CUTOUT, UPPER STRIP BROKEN AND WITH CORROSION.(FUSELAGE SECTION 48, APU INTAKE DOOR CUTOUT, UPPER STRIP WAS REPLACED IAW SRM 51-10-02-0G-0 PAR 9 REV 127 15DEC24. NO FURTHER DEFECTS NOTED.
) - [SDR UIEA2025031900244](https://openairdocs.org/sdr/UIEA2025031900244.md): Skin · damaged · Mar 15, 2025 · N1373A · Boeing 76731K · Wing, Plate/Skin > RH WING, FIXED LEADING EDGE, BETWEEN WS 538.2 AND WS 564.2 (SLAT # 9, INBOARD MAIN TRACK, CUT OUT) WITH EDGE BROKEN.(RH WING, FIXED LEADING EDGE, BETWEEN WS 538.2 AND WS 564.2 WAS REPAIRED IAW B767 SRM 57-41-01-2R-1 AND SRM 51-70-08-0G-0 PAR 5 G FIG 14 REV - [SDR UIEA2025031900243](https://openairdocs.org/sdr/UIEA2025031900243.md): Spacer · corroded · Mar 15, 2025 · N1373A · Boeing 76731K · Horizontal Stabilizer Structure > HORIZONTAL STABILIZER RH PIVOT PIN, OUTER SPACER WITH CORROSION.(
HORIZONTALSTABILIZER RH PIVOT PIN, OUTER SPACER WAS REPLACED I.A.W AMM 55-17-51-404-013 REV 144 22DEC24. NO FURTHER DEFECTS NOTED.
) - [SDR UIEA2025031900241](https://openairdocs.org/sdr/UIEA2025031900241.md): Stringer · broken · Mar 15, 2025 · N1373A · Boeing 76731K · Fuselage Main, Longeron/Stringer > BULK CARGO COMPARTMENT, BTW STA 1480 AND STA 1502, STRINGER 30L BROKEN.(BULK CARGO COMPARTMENT, BTW STA 1480 AND STA 1502, STRINGER 30L WAS REPAIRED IAW. TRE6753717 ISSUED DATE 21FEB25 FVCI EO #25037-1 REV. A. ISSUED DATE EO 20FEB25 FAA FORM 8110-3 ISSUED D - [SDR UIEA2025030800240](https://openairdocs.org/sdr/UIEA2025030800240.md): Control Module · leaking · Mar 15, 2025 · N1373A · Boeing 76731K · Flight Control System > HORIZONTAL STABILIZER WITH EVIDENCE OF HYDRAULIC LEAKAGE STAB TRIM CONTROL MODULE RH.(
LEAKAGE CHECK IN STAB TRIM CONTROL MODULE RH WAS PERFORMED IAW AMM 29-11-00-796-053 REV.144 DATE: 22DEC24. NO LEAK FOUND.
) - [SDR UIEA2025031900237](https://openairdocs.org/sdr/UIEA2025031900237.md): Door Frame · corroded · Mar 15, 2025 · N1373A · Boeing 76731K · Fuselage Main, Structure > AFT CARGO COMPARTMENT, CUT OUT LOWER DOOR, BETWEEN STA 1263 AND STA 1285, FRAME WITH CORROSION, L=2", W=1.5".(AFT CARGO COMPARTMENT, CUT OUT LOWER DOOR, BETWEEN STA 1263 AND STA 1285, FRAME CORROSION LEVEL 2 WAS REPAIRED IAW TRE 6753718 ISSIED DATE 21FEB25. - [SDR UIEA2025031900235](https://openairdocs.org/sdr/UIEA2025031900235.md): Lens · broken · Mar 15, 2025 · N1373A · Boeing 76731K · Flight Compartment Lighting > SWITCH "MAIN DECK CARGO", LENS BROKEN.(
MAIN DECK CARGO LIGHTS SWITCH LENS WAS REPLACED IAW AMM 33-34-00-900-801 REV 144 22DEC24 MAIN DECK CAR GO LIGHTS SWITCH, SATISFACTORY TEST IAW AMM 33-34-00-700-801 REV 144 22DEC24. NO FURTHER DEFECTS NOTED.
) - [SDR UIEA2025031900234](https://openairdocs.org/sdr/UIEA2025031900234.md): Skin · gouged · Mar 15, 2025 · N1373A · Boeing 76731K · Nacelle/Pylon Structure > ENG 1, LH SIDE, SKIN ON AFT TORQUE BOX WITH A GOUGE.(ENG 1, LH SIDE, SKIN ON AFT TORQUE BOX DAMAGE WAS REPAIRED IAW TRE6754205 ISSUED DATE 01MAR25. RDR NUMBER: CMA-TLS-25-0015-03B DATE 01MAR25. NO FURTHER DEFECTS
) - [SDR UIEA2025031980233](https://openairdocs.org/sdr/UIEA2025031980233.md): Bracket · corroded · Mar 15, 2025 · N1373A · Boeing 76731K · Fuselage Miscellaneous Structure > CORROSION ON PROXIMITY SENSORS BASE SUPPORT (S234, S235) AT FWD BULKHEAD OF NLG WHEEL WELL. (L= 1 IN, W= 2 IN).(PROXIMITY SENSORS BASE SUPPORT (S234, S235) AT FWD BULKHEAD OF NLG WHEEL WELL, WAS REPLACED IAW SRM 51-10-02-OG-0 PARG 9 REV 127. NO FURTHER DEFE - [SDR UIEA2025030800232](https://openairdocs.org/sdr/UIEA2025030800232.md): Elec Connector · corroded · Mar 15, 2025 · N1373A · Boeing 76731K · Electrical Power System Wiring > CORROSION ON UPPER CONNECTOR OF PROXIMITY SENSOR S234 AT FWD BULKHEAD OF NLG WHEEL WELL.(
CONNECTOR S234 WAS REPLACED IAW SWPM 20-61-00 REV 88, TEST SATISFACTORY, A/C GOOD FOR SERVICE.
) - [SDR UIEA2025030800230](https://openairdocs.org/sdr/UIEA2025030800230.md): Lamp · inoperative · Mar 15, 2025 · N1373A · Boeing 76731K · Landing Gear Brake System > REF DMI 225254 PARKING BRAKE LIGHT INOP, PARKING BRAKE LIGHTS, PARK BRAKE LIGHT 300 ANTISKID LIGHT VERIFIED OPERATIVE.(PARK BRAKE LIGHT 300 ANTISKID LIGHT VERIFIED OPERATIVE. LAMPS WERE REPLACED IAW 32-44-08-712-016 REV 114 WITH A SATISFACTORY TEST. DMI 225 - [SDR UIEA2025031980228](https://openairdocs.org/sdr/UIEA2025031980228.md): Skin · dented · Mar 15, 2025 · N1373A · Boeing 76731K · Leading Edge Devices > LEFT WING, OUTBOARD SLAT #1 IN REAR SKIN WITH DENT.(
LEFT WING, SLAT 1 T/E WEDGE, LOWER SURFACE WAS REPAIRED IAW SRM 57- 43-02-2R-1 FIG.201 PAG.2-3 AND SRM 51-70-10-2R-4 REPAIR 4 FIG.201 SHEET 2 PAG.1,4,7 REV.127. NO FURTHER DEFECTS NOTED.
) - [SDR UIEA2025031960223](https://openairdocs.org/sdr/UIEA2025031960223.md): Support · cracked · Mar 15, 2025 · N1373A · Boeing 76731K · Trailing Edge Flaps > LEFT WING TRAILING EDGE INBOARD FLAP 4 SUPPORT MECHANISM 6-6 OUTER PIN WITH CRACK INDICATION.(THE 6-6 OUTER PIN OF THE LH WING INB FLAP SUPPORT #4 WAS REPLACED IAW AMM 27-51-04-402-135 REV.144 DATE: 22DEC24 TORQUE WERE APPLIED 1000 LB/IN S/N: 0823114442 D/D - [SDR UIEA2025031900218](https://openairdocs.org/sdr/UIEA2025031900218.md): Web · corroded · Mar 15, 2025 · N1373A · Boeing 76731K · Fuselage Miscellaneous Structure > BULK CARGO COMPARTMENT, CUT OUT DOOR, BETWEEN STA 1480 AND STA 1502, INTERCOSTAL SKIN WITH CORROSION, L=2", W=1".(
BULK CARGO COMPARTMENT, CUT OUT DOOR, BETWEEN STA 1480 AND STA 1502, INTERCOSTAL SKIN WAS FABRICATED IAW. DWG / PL 146T5404 REV. E AND WAS INST - [SDR UIEA2025030190216](https://openairdocs.org/sdr/UIEA2025030190216.md): Antenna · corroded · Mar 15, 2025 · N1373A · Boeing 76731K · Air Collision Avoidance System > CORROSION ON BOTTOM TCAS ANTENNA.(
TCAS ANTENNA BOTTOM WAS REPLACED, ON P/N 071-50001-8102 S/N 582-34534, OFF P/N 071-50001-8102 S/N TLS33506. TEST SATISFACTORY. IAW. AMM 34-45-02-344-160 REV 144 DATE 22DEC24. TORQUE APPLIED 22.5 IN.LB S/N 924401137 DATE 30S - [SDR UIEA2025030600215](https://openairdocs.org/sdr/UIEA2025030600215.md): Bolt · corroded · Mar 15, 2025 · N1373A · Boeing 76731K · Turbine Engine Air Inlet Section > ENG 2, FAN CASE, OGVS BOLTS AREA, 113 BOLTS, BETWEEN 7 - 11 WITH CORROSION.(
ENG 2, FAN CASE, OGVS BOLTS AREA, 113 BOLTS, BETWEEN 7 - 11, CORROSION WAS EVALUATED, REMOVED, AND PERFORMED DVI, FOUND TO BE WITHIN ALLOWABLE DAMAGE LIMITS IAW. AMM 72-33-00-206-00 - [SDR UIEA2025030190204](https://openairdocs.org/sdr/UIEA2025030190204.md): Retainer · corroded · Mar 15, 2025 · N1373A · Boeing 76731K · Fuselage Miscellaneous Structure > CORROSION ON FWD SEAL RETAINER AT FWD BULKHEAD AT NLG WHEEL WELL. (BELOW TO PROXIMITY SENSORS S234, S235) (L= 4 IN, W= 0.5 IN).(
FWD SEAL RETAINER AT FWD BULKHEAD AT NLG WHEEL WELL. (BELOW TO PROXIMITY SENSORS S234, S235), WAS REPLACED IAW. SRM 51-10-02-0G-0 - [SDR UIEA2025030400203](https://openairdocs.org/sdr/UIEA2025030400203.md): Retainer · corroded · Mar 15, 2025 · N1373A · Boeing 76731K · Fuselage Miscellaneous Structure > CORROSION ON LH SEAL RETAINER AT FWD BULKHEAD AT NLG WHEEL WELL. (NEXT TO PROXIMITY SENSOR S256) (L= 4 IN, W= 0.5 IN).(
LH AT FWD BULKHEAD AT NLG WHEEL WELL SEAL RETAINER WAS REPLACED IAW SRM 51-10-02-0G-0 PAR 9 REV 127. NO FURTHER DEFECTS NOTED. - [SDR UIEA2025030194202](https://openairdocs.org/sdr/UIEA2025030194202.md): Case · corroded · Mar 15, 2025 · N1373A · Boeing 76731K · Turbine Engine Air Inlet Section > ENG 1, FWD FAN CASE, AT 6 O'CLOCK APPROX, FWD MATING FLANGE WITH SEVERAL POINTS OF CORROSION (2EA).(
ENG 1, FWD FAN CASE, AT 6 O'CLOCK APPROX, FWD MATING FLANGE CORROSION LEVEL 1 WERE REWORKED, EVALUATED, INSPECTED AND FOUND TO BE WITHIN ALLOWABLE LIMITS IAW - [SDR UIEA2025030194201](https://openairdocs.org/sdr/UIEA2025030194201.md): Skin · cracked · Mar 15, 2025 · N1373A · Boeing 76731K · Fuselage Main, Plate/Skin > FWD ENTRY DOOR, AFT LOWER CORNER, CRACK INDICATION AT HOLE 3 ON SKIN AT APPROX 10 O´CLOCK. AND CRACK INDICATION AT HOLE 4, THROUGH THE HOLE (SKIN AND BEAR STRAP) APPROX. 10 O´CLOCK AND CROSS DOWN.(
FWD ENTRY DOOR, AFT LOWER CORNER, CRACK INDICATION AT HOLE - [SDR UIEA2025030400200](https://openairdocs.org/sdr/UIEA2025030400200.md): Wedge · dented · Mar 15, 2025 · N1373A · Boeing 76731K · Leading Edge Devices > LEFT WING, SLAT 6 INBOARD FACE, TRAILING EDGE WEDGE WITH DENT APRX 42€Œ OF OUTBOARD EDGE.(
LEFT WING, SLAT 6 INBOARD FACE, T/E WEDGE AT APRX 42" OF OUTBOARD EDGE WAS REPAIRED IAW SRM 57-43-02-2R-1 FIG.201 PAG.2-3 AND SRM 51-70-10-2R-4 REPAIR 4 FIG. 201 SHEE - [SDR UIEA2025030400199](https://openairdocs.org/sdr/UIEA2025030400199.md): Wedge · bent · Mar 15, 2025 · N1373A · Boeing 76731K · Leading Edge Devices > LEFT WING, SLAT 6 INBOARD FACE WITH BENT APRX 50€Œ OF INBOARD EDGE.(
LEFT WING, SLAT 6 T/E WEDGE INBOARD FACE AT APRX 50" OF INBOARD EDGE WAS REPAIRED IAW SRM 57-43-02-2R-1 FIG. 201 PAG.2-3 AND SRM 51-70-10-2R-4 REPAIR 4 FIG. 201 SHEET 2. NO FURTHER DEFECTS - [SDR UIEA2025030400198](https://openairdocs.org/sdr/UIEA2025030400198.md): Skin · cracked · Mar 15, 2025 · N1373A · Boeing 76731K · Fuselage Main, Plate/Skin > FWD SERVICE DOOR, AFT LOWER CORNER, CRACK INDICATION AT HOLE 3 ON SKIN AT APPROX 2 O´CLOCK AND CRACK INDICATION AT HOLE 4, THROUGH THE HOLE (SKIN AND BEAR STRAP) APPROX. 2 O´CLOCK AND CROSS DOWN AND AT 4 O´CLOCK.(
CRACK AT HOLE 4 THROUGH THE HOLE APROX. 2
- [SDR UIEA2025022500165](https://openairdocs.org/sdr/UIEA2025022500165.md): Bracket · corroded · Mar 15, 2025 · N1373A · Boeing 76731K · Horizontal Stabilizer Miscellaneous Structure
> HORIZONTAL STABILIZER ENTER SECTION, UPPER SURFACE, LBL 41.5 AND BETWEEN REAR SPAR AND S-1, BRACKET WITH CORROSION.
(
HORIZONTAL STABILIZER ENTER SECTION, UPPER SURFACE, LBL 41.5 AND BETWEEN REAR SPAR AND S-1, BRACKET WAS REPLACED IAW SRM 51-10-02-0G-0 PA - [SDR UIEA2025022500164](https://openairdocs.org/sdr/UIEA2025022500164.md): Frame · corroded · Mar 15, 2025 · N1373A · Boeing 76731K · Fuselage Main, Frame > BULK CARGO COMPARTMENT, AT STA 1518, BTW STRG 28L AND 29L FRAME WITH CORROSION (L=2" W=1.5").(
BULK CARGO COMPARTMENT, AT STA 1518, BTW STRG 28L AND 29L FRAME, CORROSION LEVEL 1 WAS EVALUATED. REWORKED, AND INSPECTED, FOUND TO BE WITHIN ALLOWABLE DAMAGE LIMI - [SDR UIEA2025022500163](https://openairdocs.org/sdr/UIEA2025022500163.md): Support · corroded · Mar 15, 2025 · N1373A · Boeing 76731K · Fuselage Miscellaneous Structure > CORROSION ON LH ANGLE STRAP SUPPORT (NEXT TO PROXIMITY SENSOR S256 CONNECTOR BOX) AT LH MID SIDE AREA OF FWD BULKHEAD AT NLG WHEEL WELL. (L= 0.260 IN, W= 0.1 IN)(
CORROSION LEVEL 1 WAS REMOVED, EVALUATED, INSPECTED, AND FOUND TO BE IN ALLOWABLE DAMAGE LIMITS - [SDR UIEA2025022500162](https://openairdocs.org/sdr/UIEA2025022500162.md): Case · corroded · Mar 15, 2025 · N1373A · Boeing 76731K · Turbine Engine Air Inlet Section > ENG 2, FAN CASE AREA AT 6 O´CLOCK POSITION, AROUND THE ANCHORED NUT WITH CORROSION.(
ENG 2, FAN CASE AREA AT 6 O´CLOCK POSITION, AROUND THE ANCHORED NUT WAS REMOVED, CORROSION LEVEL 1 WAS REWORKED, INSPECTED, EVALUATED AND ALLOWABLE LIMITS FOUND IAW AMM 72 - [SDR UIEA2025022500161](https://openairdocs.org/sdr/UIEA2025022500161.md): Fitting · corroded · Mar 15, 2025 · N1373A · Boeing 76731K · Fuselage Miscellaneous Structure > CORROSION AT LH LOWER FITTING ON FWD BULKHEAD OF NLG WHEEL WELL. (L= 0.1 IN, W= 0.2 IN)(
CORROSION LEVEL 1 WERE REMOVED, EVALUATED, INSPECTED AND FOUND TO BE WITHIN ALLOWABLE DAMAGE LIMITS AT LH LOWER FITTING ON FWD BULKHEAD OF NLG WHEEL WELL IAW SRM 53-10-0 Next page: https://openairdocs.org/aircraft/N1373A/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 = 'N1373A' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N1373A/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.