RH WING, SLAT 11 WAS REPAIRED IAW SRM 57-43-02-2R-1 REP 1 PAGE 2-3 FIG 201 AND SRM 51-70-1 OOR REP 4 PAGE 1-7 FIG 201 (SHEET 2) REV 127. 15-DEC-24. NO FURTHER DEFECTS NOTED
) - [SDR UIEA2025011300053](https://openairdocs.org/sdr/UIEA2025011300053.md): Line · leaking · Jan 22, 2025 · N1399A · Boeing 767306 · Hydraulic System, Main > ENG 2 NACELLE STRUT LINE WITH LEAK.(ENG 2 NACELLE STRUT LINE WITH LEAK, TORQUE WAS APPLIED 127 LB-IN SN:1017801833
/DATE: 11-APR-25 IAW AMM: 71-00-02-404-049-H03 REV.144 DATE: 22-DEC-2024. LEAK CHECK WAS GOOD.
) - [SDR UIEA2025011600068](https://openairdocs.org/sdr/UIEA2025011600068.md): Strip · corroded · Jan 22, 2025 · N1399A · Boeing 767306 · Nacelle/Pylon Miscellaneous Structure > ENG 1, RH CORE COWL, UPPER STRIP WITH CORROSION. L: 2.500 IN, W: 1.000 IN.(THE CORROSION METAL STRIP WAS REMOVED, THE NEW METAL STRIP WAS DRILLED AND WAS INSTALLED CORRECTLY. SRM 51-40-02-0G-0 REV 127 15DEC24 AND SRM 51-10-02-0G-0 PAR 9. LEVEL 1. NO FURTHER - [SDR UIEA2025011600070](https://openairdocs.org/sdr/UIEA2025011600070.md): Orifice · obstructed · Jan 22, 2025 · N1399A · Boeing 767306 · Smoke Detection > AFT AND BULK CARGO COMPATMENT CARGO SMOKE DET AIR SAMPLING ORIFICES BLOCKED AND DIRTY.(
SMOKE DET AIR SAMPLING ORIFICES WERE CLEANED IAW 26-05-03-202-001 REV 143 22AUG24. NO FURTHER DEFECTS NOTED
) - [SDR UIEA2025011600071](https://openairdocs.org/sdr/UIEA2025011600071.md): Pca · leaking · Jan 22, 2025 · N1399A · Boeing 767306 · Aileron Control System > RIGHT WING INBOARD AILERON, PCA´S WITH LEAK EVIDENCE.(RIGHT WING INBOARD AILERON, PCA´S LH, AND RH WERE REPLACED I.A.W AMM 27-11-48-022-003. NO FURTHER DEFECTS NOTED
) - [SDR UIEA2025011600072](https://openairdocs.org/sdr/UIEA2025011600072.md): Orifice · obstructed · Jan 22, 2025 · N1399A · Boeing 767306 · Smoke Detection > FWD CARGO COMPARTMENT CARGO SMOKE DET AIR SAMPLING INTAKE ORIFICES BLOCKED AND DIRTY.(FWD CARGO COMPARTMENT CARGO SMOKE DET AIR SAMPLING INTAKE ORIFICES WERE CLEANED IAW AMM 26-05-03-202-001 REV 143. NO FURTHER DEFECTS NOTED
) - [SDR UIEA2025011600073](https://openairdocs.org/sdr/UIEA2025011600073.md): Access Panel · loose · Jan 22, 2025 · N1399A · Boeing 767306 · Nacelle/Pylon, Plate/Skin > ENG 1, INNER ACCESS PANEL 432 FL, PIPE "FIRE PROTECTION" WITH NUT LOOSE.(ENG 1, INNER ACCESS PANEL 432 FL, PIPE "FIRE PROTECTION" NUT WAS TORQUED AND VERIFIED IAW AMM 20-11-00-910-801. NO FURTHER DEFECTS NOTED
) - [SDR UIEA2025011600074](https://openairdocs.org/sdr/UIEA2025011600074.md): Access Panel · misinstalled · Jan 22, 2025 · N1399A · Boeing 767306 · Smoke Detection > ACCESS PANEL OF MAIN DECK CARGO SMOKE DETECTOR WAS INSTALLED WRONG. (CCD ZONE 121)(CARGO SMOKE DETECTOR ACCESS PANEL WAS INSTALLED CORRECTLY IAW AMM 23-16-01-400-801-061 - [SDR UIEA2025011600075](https://openairdocs.org/sdr/UIEA2025011600075.md): Fuel Cell · leaking · Jan 22, 2025 · N1399A · Boeing 767306 · Fuel Storage > FUEL LEAK ON LEFT WING LWR SIDE OF BODY SPLICE PLATE AT STRINGER L-6 AND WBL 97.5 APROX.(
FUEL LEAK ON LEFT WING LWR SIDE OF BODY SPLICE PLATE AT STRINGER L-6 AND WBL 97.5 APROX. THE AREA WAS VENTILATED, THE REMAINING FUEL WAS CLEANED, THE SEALANT IS REMOVED - [SDR UIEA2025011600076](https://openairdocs.org/sdr/UIEA2025011600076.md): Fuel Cell · leaking · Jan 22, 2025 · N1399A · Boeing 767306 · Fuel Storage > FUEL LEAK EVIDENCE, LH WING LOWER SIDE AT BODY SPLICE AND STRINGER 10 AND 15.(
THE AREA WAS VENTILATED, THE REMAINING FUEL WAS CLEANED, THE SEALANT WAS REMOVED, THE AREA WAS CLEANED CORRECTLY, CLASS "A" AND CLASS "B" SEALANT WAS APPLIED CORRECTLY, THE FUEL L
- [SDR UIEA2025011600077](https://openairdocs.org/sdr/UIEA2025011600077.md): Structure · none · Jan 22, 2025 · N1399A · Boeing 767306 · Standard Practices/Structures
> CONTAMINATED EWIS WITH CIC OF NOSE LANDING GEAR WHEEL WELL.
(
NOSE LANDING GEAR WHEEL WELL EWIS WAS CLEANED IAW SWPM 20-10-04 REV 87. NO FURTHER DEFECTS NOTED
) - [SDR UIEA2025011600078](https://openairdocs.org/sdr/UIEA2025011600078.md): Skin · delaminated · Jan 22, 2025 · N1399A · Boeing 767306 · Trailing Edge Flaps > LH WING, L/E OUTBD FLAP, FROM INBD EDGE TO 58 INCHES TO OUTSIDE WITH DELAMINATION.(LH WING, L/E OUTBD FLAP, FROM INBD EDGE TO 58 INCHES WAS REPAIRED IAW SRM 57-53-01-2R-1 FIG 10 AND SRM 51-70-17-17-0G-0 PAR.4.A REV 127. NO FURTHER DEFECTS NOTED
) - [SDR UIEA2025011700080](https://openairdocs.org/sdr/UIEA2025011700080.md): Acoustic Panel · corroded · Jan 22, 2025 · N1399A · Boeing 767306 · Nacelle/Pylon, Main Frame > ENGINE 2, AIR INLET COWL, ACOUSTICAL PANEL AT 7 TO 8 O'CLOCK POSITION WITH EVIDENCE OF CORROSION.(ENGINE 2, AIR INLET COWL, ACOUSTICAL PANEL AT 7 TO 8 O'CLOCK POSITION WITH EVIDENCE OF LEVEL 2 CORROSION WAS REPLACED IAW AMM 71-11-01-404-005-H00 REV 144. NO - [SDR UIEA2025011700081](https://openairdocs.org/sdr/UIEA2025011700081.md): Lens · broken · Jan 22, 2025 · N1399A · Boeing 767306 · Emergency Lighting > BROKEN EMERGENCY LIGHT ON FWD LH PASSENGER DOOR.(
LINING INSTL- FWD ENTRY DOOR, FWD SIDE DOORWAY LENS (EXIT) WAS INSTALLED IAW AMM 33-51-01-400-801-001. OPS CHK OK
) - [SDR UIEA2025011700082](https://openairdocs.org/sdr/UIEA2025011700082.md): Structure · none · Jan 22, 2025 · N1399A · Boeing 767306 · Standard Practices/Structures > MISSING CIC ON SEVERAL AREAS OF NOSE LANDING GEAR WHEEL WELL.(MISSING CIC ON SEVERAL AREAS OF NOSE LANDING GEAR WHEEL WELL. DAMAGED CIC WAS REMOVED AND AREA CLEANED FOR APPLICATION, CIC IS APPLIED CORRECTLY. AMM 51-24-09-377-008 REV 143 AND AMM 51-24-09-917 - [SDR UIEA2025011700083](https://openairdocs.org/sdr/UIEA2025011700083.md): Fuel Tank · leaking · Jan 22, 2025 · N1399A · Boeing 767306 · Fuel Storage > FUEL LEAK ON RIGHT WING LWR SIDE OF BODY SPLICE PLATE AT STRINGER L-15 AND WBL 97.5 APROX.(
THE SEALANT IS REMOVED, THE AREA IS CLEANED CORRECTLY, CLASS "A" AND CLASS "B" SEALANT IS APPLIED CORRECTLY AND THE FUEL LEAK TEST PERFORMED WAS SATISFACTORY. AMM 28- - [SDR UIEA2025011700084](https://openairdocs.org/sdr/UIEA2025011700084.md): Retainer · corroded · Jan 22, 2025 · N1399A · Boeing 767306 · Landing Gear Doors > MAIN LANDING GEAR DOOR RH, TRACK OF SEAL BULB AFT, WITH EVIDENCE WITH CORROSION.(
MAIN LANDING GEAR DOOR RH, TR ACK OF SEAL BULB AFT, WITH EVIDENCE WITH CORROSION, WAS REPLACED IAW SRM 51-10-02-0G-0 REV 127. NO FURTHER DEFECTS NOTED
) - [SDR UIEA2025011800086](https://openairdocs.org/sdr/UIEA2025011800086.md): Support Angle · cracked · Jan 22, 2025 · N1399A · Boeing 767306 · Nacelle/Pylon Miscellaneous Structure > BROKEN ENG 2, ACCESS PANEL 447DB, ANGLE SUPPORT WITH CRACK.(THE BROKEN SUPPORT ANGLE WAS REMOVED, THE AREA WAS CLEANED, THE NEW SUPPORT ANGLE WAS DRILLED AND INSTALLED CORRECTLY. THE SUPPORT ANGLE WAS REPLACED WITH A NEW ONE. DWG 313T3360 SRM 51-40-02-OG-O - [SDR UIEA2025012000090](https://openairdocs.org/sdr/UIEA2025012000090.md): Pca · leaking · Jan 22, 2025 · N1399A · Boeing 767306 · Aileron Control System > LH WING INBOARD AILERON INBOARD PCA WITH EVIDENCE HYDRAULIC LEAK.(
INBOARD PCA WAS REPLACED I.A.W. AMM 27- 11-48-422-040, REV. 144, DATE: DEC. 22, 2024. TORQUE APPLIED: ROD END: 1200 IN- LB, S/N: 0808504320. INBOARD AILERON ADJUSTMENT AND OPERATIONAL TEST WE - [SDR UIEA2025012000091](https://openairdocs.org/sdr/UIEA2025012000091.md): Skin · cracked · Jan 22, 2025 · N1399A · Boeing 767306 · Fuselage Main, Plate/Skin > FORWARD ENTRY DOOR CUTOUT AFT LOWER CORNER WITH TWO CRACK INDICATIONS AT HOLE 2 ON SKIN, POSITION 11 O´CLOCK AND 5 O'CLOCK, SEE N.D.T. INSPECTION REPORT.(
TWO CRACK INDICATIONS AT HOLE 2 ON SKIN, POSITION 11 O´CLOCK AND 5 O'CLOCK, WERE REPAIRED IAW SRM 53- - [SDR UIEA2025012000092](https://openairdocs.org/sdr/UIEA2025012000092.md): Skin · cracked · Jan 22, 2025 · N1399A · Boeing 767306 · Fuselage Main, Plate/Skin > FUSELAGE - SECTION 41 - SERVICE DOOR CUTOUT AFT LOWER CORNER WITH A CRACK INDICATION AT HOLE 2 ON SKIN AND BEAR STRAP, POSITION 2 O´CLOCK, SEE N.D.T. INSPECTION REPORT.(
CRACK ON RH FUSELAGE, R1 DOOR CUTOUT, AFT LOWER CORNER ON SKIN WAS REPAIRED IAW SRM 53- - [SDR UIEA2025012000093](https://openairdocs.org/sdr/UIEA2025012000093.md): Fuel Cell · leaking · Jan 22, 2025 · N1399A · Boeing 767306 · Fuel Storage > FUEL LEAK ON LEFT WING LWR SIDE OF BODY SPLICE PLATE AT STRINGER L-15 AND WBL 97.5 APROX.(
FUEL LEAK ON LEFT WING LWR SIDE OF BODY SPLICE PLATE AT STRINGER L- 15 AND WBL 97.5 APROX. SEALANT WAS REMOVED AND REPLACED. CLASS "A" AND CLASS "B" SEALANT WAS INSTAL - [SDR UIEA2025012000094](https://openairdocs.org/sdr/UIEA2025012000094.md): Servo · leaking · Jan 22, 2025 · N1399A · Boeing 767306 · Flight Control System > VERTICAL STABILIZER, REAR SPAR, YAW DAMPER SERVOS ASSY, LEAKING EVIDENCE.(
YAW DAMPER SERVOS LEFT AND RIGHT, WERE REPLACED, TEST WERE PERFORMED AND HYD LEAKAGE CHECK WAS PERFORMED AND TORQUE WAS APPLIED IAW AMM 22-21-02-414-016 REV 143. OPS CHECK GOOD.
) - [SDR UIEA2025012000095](https://openairdocs.org/sdr/UIEA2025012000095.md): Pcu · leaking · Jan 22, 2025 · N1399A · Boeing 767306 · Elevator Control System > LH ELEVATOR, PCU'S LEAKING EVIDENCE.(LH ELEVATOR, INBOARD, AND OUTBOARD PCA WERE REPLACED IAW AMM 29-31-05-424-027 REV144. TORQUE APPLIED: 200 LB-IN, 270 LB-IN S/N:040674400. ADJUSTMENT WAS PERFORMED. OPERATIONAL TEST WAS SATISFACTORY.
) - [SDR UIEA2025012100098](https://openairdocs.org/sdr/UIEA2025012100098.md): Frame · corroded · Jan 22, 2025 · N1399A · Boeing 767306 · Nacelle/Pylon, Main Frame > ENGINE 2 AIR INLET COWL, FAN FRAME, AROUND AT 7 TO 8 O CLOCK POSITION WITH CORROSION.(ENG 2 INLET COWL WAS REPLACED IAW 71-11-01-404-005-H00 REV 144. NO FURTHER DEFECTS NOTED
) - [SDR UIEA2025012100099](https://openairdocs.org/sdr/UIEA2025012100099.md): Skin · worn · Jan 22, 2025 · N1399A · Boeing 767306 · Leading Edge Devices > RH WING, SLAT # 7, WORN LOWER SKIN.(RH WING, SLAT 7 LOWER SKIN WAS REPAIRED I.A.W SRM 57-43-02-2R-1 PG 1-3 FIG 201 AND SRM 51-70-10-2R-4 PG 1,15 FIG 202 SHEET 8 REV 127 15-DEC-24. NO FURTHER DEFECTS NOTED
) - [SDR UIEA2025012100100](https://openairdocs.org/sdr/UIEA2025012100100.md): Frame · corroded · Jan 22, 2025 · N1399A · Boeing 767306 · Turbine Engine Air Inlet Section > ENG 1, FAN FRAME, BTWN 4-8 O'CLOCK SURFACE WITH SEVERAL POINTS OF CORROSION.(ENG 1, FLOWPATH EXTENSION BETWEEN 4 TO 8 O'CLOCK WERE REPLACED IAW AMM 72-33-00-308-104-H00 REV 144. NO FURTHER DEFECTS NOTED
) - [SDR UIEA2025012100101](https://openairdocs.org/sdr/UIEA2025012100101.md): Pcu · leaking · Jan 22, 2025 · N1399A · Boeing 767306 · Elevator Control System > RH ELEVATOR PCU'S LEAKING EVIDENCE.(RH ELEVATOR, INBOARD, AND OUTBOARD PCA WERE REPLACED IAW AMM 29-31-05-424-027 REV 144. TORQUE WAS APPLIED: 200 LB-IN, 270 LB-IN S/N: 0406744400. ADJUSTMENT WAS PERFORMED. OPERATIONAL TEST WAS SATISFACTORY.
) - [SDR UIEA2024111301084](https://openairdocs.org/sdr/UIEA2024111301084.md): Warning Message · false indication · Nov 13, 2024 · N1399A · Boeing 767306 · Hydraulic Pump (Electric/Engine), Main > ON APPROACH CENTER PRIMARY HYD PUMP #1 EICAS MSG(PERFORMED TROUBLESHOOTING AND OPS CHECKS IAW FIM 29-11 FAULT TREE 810. OPS CHECK GOOD, NO C/B'S POPPED, COULD NOT DUPLICATE. NO FURTHER MX REQUIRED.
) - [SDR UIEA2024080200766](https://openairdocs.org/sdr/UIEA2024080200766.md): Bulb · inoperative · Aug 2, 2024 · N1399A · Boeing 767306 · Emergency Equipment > BACKLIGHTING FOR EMERG LIGHT PAX OXY PANEL ONLY 1/2 ILLUMINATED. REPAIRED LIGHTPLATE & REPLACED BULBS PER SWPM 20-40-00. OPS CK OK PER 33-13-01. - [SDR UIEA2023122901045](https://openairdocs.org/sdr/UIEA2023122901045.md): Unknown · unknown · Dec 30, 2023 · N1399A · Boeing 767306 · Cargo/Baggage Doors > MAIN DECK CARGO DOOR, ZONE 838 WITH PRESSURIZATION LEAKS.(LEAKS WERE EVALUATED AND FOUND WITHIN ALLOWABLE LIMITS IAW AMM 05-51-24-782-001
) - [SDR UIEA2023123001052](https://openairdocs.org/sdr/UIEA2023123001052.md): Stringer Splice · unknown · Dec 30, 2023 · N1399A · Boeing 767306 · Fuselage Main, Longeron/Stringer > MDC UPPEN MAIN - AUX SILLS SPLICE TO STRINGERS - BETWEEN STA 412 TO STA 434 ON STRINGER 13, CRACK INDICATION FOUND.(STRINGER SPLICE WAS REPLACED IAW DRAWING 311T1130 & FVCI #23238-1 REV A. NO FURTHER DEFECTS NOTED
) - [SDR UIEA2023123001051](https://openairdocs.org/sdr/UIEA2023123001051.md): Stringer Splice · unknown · Dec 30, 2023 · N1399A · Boeing 767306 · Fuselage Main, Longeron/Stringer > MDC UPPEN MAIN - AUX SILLS SPLICE TO STRINGERS - BETWEEN STA 412 TO STA 434 ON STRINGER 17, CRACK INDICATION FOUND.(STRINGER SPLICE WAS REPLACE IAW DRAWING 311T1130, FVCI #23238-1 REV A. NO FURTHER DEFECTS NOTED
) - [SDR UIEA2023123001050](https://openairdocs.org/sdr/UIEA2023123001050.md): Stiffener · unknown · Dec 30, 2023 · N1399A · Boeing 767306 · Nacelle/Pylon, Main Frame > NACELLE STRUT #2 UPPER SPAR WEB CRACK IN LH STIFFENER NAC STA 196.86 (JUST BELOW UPPER LINK)(R/R STIFFENER IAW BOEING DRAWING 311T1130. NO FURTHER DEFECTS NOTED.
) - [SDR UIEA2023122901047](https://openairdocs.org/sdr/UIEA2023122901047.md): Unknown · unknown · Dec 30, 2023 · N1399A · Boeing 767306 · Cargo/Baggage Doors > FWD CARGO DOOR, ZONE 821 WITH PRESSURIZATION LEAKS(LEAKS WERE EVALUATED AND FOUND WITHIN THE ALLOWABLE LIMITS IAW AMM 05-51-24-782-001
) - [SDR UIEA2023122901046](https://openairdocs.org/sdr/UIEA2023122901046.md): Unknown · unknown · Dec 30, 2023 · N1399A · Boeing 767306 · Cargo/Baggage Doors > MAIN DECK CARGO DOOR, ZONE 838 WITH PRESSURIZATION LEAKS.(PRESSURIZATION LEAKS WERE EVALUATED AND FOUND WITHIN THE ADL IAW AMM 05-51-24-782-001
) - [SDR UIEA2023122901044](https://openairdocs.org/sdr/UIEA2023122901044.md): Unknown · unknown · Dec 30, 2023 · N1399A · Boeing 767306 · Fuel Storage > RH WING FUEL LEAK STA 642.20 & 668.20(FUEL LEAKS WERE CORRECTED IAW AMM 28-11-00-308-013. NO FURTHER DEFECTS NOTED
) - [SDR UIEA2023122901043](https://openairdocs.org/sdr/UIEA2023122901043.md): Unknown · unknown · Dec 30, 2023 · N1399A · Boeing 767306 · Landing Gear Brake System > TAT & AUTO BRAKE OVERHEAD ANNUNCIATER LIGHT STICK IN ANY ONLY ILLUMINATE INTERMITTENTLY(ANNUNCIATER LIGHT STICK IN ANY ONLY ILLUMINATE INTERMITTENTLY WERE REPLACED IAW AMM 33-13-00-902-024. OPS CHECK GOOD
) - [SDR UIEA2023122901042](https://openairdocs.org/sdr/UIEA2023122901042.md): Unknown · unknown · Dec 30, 2023 · N1399A · Boeing 767306 · Service Doors > AFT SERVICE DOOR, ZONE 843 WITH PRESSURIZATION LEAKS(LEAKS WERE EVALUATED AND FOUND WITHIN ADL IAW AMM 05-51-24-782-001
) - [SDR UIEA2023122901040](https://openairdocs.org/sdr/UIEA2023122901040.md): Unknown · unknown · Dec 30, 2023 · N1399A · Boeing 767306 · Passenger/Crew Doors > AFT ENTRY DOOR, ZONE 833 WITH PRESSURIZATION LEAKS.(FUEL LEAKS WERE EVALUATED AND FOUND WITHIN LIMITS IAW AMM 05-51-24-782-001 REV 140 DATE 22 AUG 23
) - [SDR UIEA2023122901039](https://openairdocs.org/sdr/UIEA2023122901039.md): Unknown · unknown · Dec 30, 2023 · N1399A · Boeing 767306 · Service Doors > FWD SERVICE DOOR, ZONE 841 WITH PRESSURIZATION LEAKS.(THE PRESSURIZATION LEAKS WERE EVALUATED AND FOUND WITHIN ADL IAW AMM 05-51-24-782-001
) - [SDR UIEA2023122901038](https://openairdocs.org/sdr/UIEA2023122901038.md): Unknown · unknown · Dec 30, 2023 · N1399A · Boeing 767306 · Passenger/Crew Doors > FWD ENTRY DOOR, ZONE 831 WITH PRESSURIZATION LEAKS(SEAL WAS REPAIRED IAW AMM 05-51-24-782-001. NO FURTHER DEFECTS NOTED
) - [SDR UIEA2023122701034](https://openairdocs.org/sdr/UIEA2023122701034.md): Module · unknown · Dec 30, 2023 · N1399A · Boeing 767306 · Fire Protection System > IN THE OPERATIONAL CHECK OF CARGO FIRE EXTINGUISHING BOTTLE, RELAYS THE AFT ARM SWITCH FOUND INOPERATIVE.(TASK CARD A-26-016-00-01/002. CARGO FIRE EXT BOTTLE RELAY AFT CARGO WAS ACCOMPLISHED IAW TASK CARD A-26-016-00-01/001 (NR00509) AND MODULE ASSY MASTER - [SDR UIEA2023122701033](https://openairdocs.org/sdr/UIEA2023122701033.md): Relay · unknown · Dec 30, 2023 · N1399A · Boeing 767306 · Extinguishing System > IN THE OPERATIONAL CHECK OF CARGO FIRE EXTINGUISHING BOTTLE RELAYS, THE RELAY K823 FOUND INOPERATIVE.(
THE RELAY K823 WAS REPLACED IAW SWPM 20-81-22 REV.84 DATE:15-OCT-23. NO FURTHER DEFECTS NOTED
) - [SDR UIEA2023122701032](https://openairdocs.org/sdr/UIEA2023122701032.md): Cap · unknown · Dec 30, 2023 · N1399A · Boeing 767306 · Pneumatic System > ENG #2, PRSOV AIR FILTER CAPS WITH CORROSION 2EA (N/P 727576-1)(ENG RH, THE CAPS OF PRSOV HAS BEEN REPLACED AND INSTALLED IAW AMM B767 36-11-09-402-114-001 REV 140 - 22 AUG 2023, THE CAPS HAS BEEN TIGHTENED TO 70 LB IN, TORQUE WRENCH: 0616601964, NEXT CALIB - [SDR UIEA2023122701031](https://openairdocs.org/sdr/UIEA2023122701031.md): Unknown · unknown · Dec 30, 2023 · N1399A · Boeing 767306 · Leading Edge Devices > BULGE ON RH WING SLAT# 9 T/E WEDGE LOWER SKIN AT OSS 603.74 AND 5" FROM T/E(
RH WING SLAT #9 T/E WEDGE LOWER SKIN WAS REPAIRED IAW SRM 57-43-02-2R-1 FIG 201 SHEET 2 PAGE1-3 AND SRM 51-70-10-2R-4 PAGE1-4 & 7 FIG 201 REV 124 DEC 15/2023
) - [SDR UIEA2023122701030](https://openairdocs.org/sdr/UIEA2023122701030.md): Unknown · unknown · Dec 30, 2023 · N1399A · Boeing 767306 · Leading Edge Devices > DENT ON RH WING SLAT# 7 T/E WEDGE UPPER SKIN AT ISS 152.38 AND 6.5" FROM T/ E(RH WING SLAT #7 T/E WEDGE UPPER SKIN WAS REPAIRED IAW SRM 57-43-02-2R-1 FIG 201 SHEET 2 PAGE 2-3 AND SRM 51-70-10-2R-4 FIG 201 SHEET 1 PAGE 1-3 & 22 REV 124 DEC 15/2023
/Next page: https://openairdocs.org/aircraft/N1399A/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 = 'N1399A' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N1399A/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.