RIGHT STAB TRIM LIMIT SWITCH/POSITION INDICATOR EXPERIENCED AN INTERNAL SHORT. R&R R/H STAB TRIM LIMIT SWITCH AND POSITION TRANSMITTER MODULE PER A - [SDR UIEA2026100900972](https://openairdocs.org/sdr/UIEA2026100900972.md): Failsafe · damaged · Oct 10, 2026 · N649GT · Boeing 767375 · Fuselage Main, Structure > DETECTED DEFECT INDICATION DURING EO 6753A070 (SB 767-53A0100 R3/AD 2021-09-04) STA 955 REAR SPAR BULKHEAD SIDE FITTING FAILSAFE STRAP ULTRASONIC INSPECTION. DEFECT SIGNAL LOCATION: FAILSAFE STRAP (RH)(
REMOVED PLATE ASSY OF R/H MAIN L/G W/W LONGN AND L/G BE - [SDR UIEA2026100900973](https://openairdocs.org/sdr/UIEA2026100900973.md): Skin · cracked · Oct 10, 2026 · N649GT · Boeing 767375 · Fuselage Main, Plate/Skin > DURING EO 6753A070 (SB 767-53A0100 R3/AD 2012-09-04 TERMINATING ACTION) OPEN-HOLE HFEC AT STA 955 R/H, A CRACK INDICATION WAS FOUND AT THE FAIL-SAFE STRAP, AND CORROSION WAS FOUND ON THE T-FITTING AND SKIN PANEL (P/N 145T3321-4) NEAR STR 22AR. REMAINING THICK - [SDR UIEA2026100900974](https://openairdocs.org/sdr/UIEA2026100900974.md): Tee Fitting · cracked · Oct 10, 2026 · N649GT · Boeing 767375 · Fuselage Main, Structure > DURING EO 6753A070 PART 4 (SB 767-53A0100 R3 / AD 2012-09-04 TERMINATING ACTION) AT STA 955 R/H, CRACKS WERE FOUND AT THE 10 O'CLOCK (0.5€?) AND 4 O'CLOCK (NOT MEASURABLE) POSITIONS FROM THE LOWEST FAIL-SAFE STRAP HOLE PER 767 NDTM 51-00-16 / 51-00-19.(
STR - [SDR UIEA2026100900975](https://openairdocs.org/sdr/UIEA2026100900975.md): Skin · corroded · Oct 10, 2026 · N649GT · Boeing 767375 · Trailing Edge Flaps > CORROSION FOUND ON R/H INBOARD MAIN FLAP LOWER SKIN (DAMAGE SIZE: L=11.2", W=1.7")(
REPAIRED THE R/H INBD MAIN FLAP LOWER PANEL (P/N 113T2243-2) SKIN IN ACCORDANCE WITH BMN SP1-TLS-26-0036, WHICH WAS APPROVED BY FAA FORM 8100-9 DATED 08OCT2026. NO FURTHER DE - [SDR UIEA2026100900976](https://openairdocs.org/sdr/UIEA2026100900976.md): Structure · corroded · Oct 10, 2026 · N649GT · Boeing 767375 · Trailing Edge Flaps > CORROSION FOUND ON L/H INBOARD MAIN FLAP LOWER CHORD (DAMAGE SIZE: L=19")(
PER BOEING RDR SP1-TLS-26-0037-05B, INSTALLATION OF CHORD (P/N 113T2225-401) ON THE FLAP (P/N 113T2201-23A) FOR AIRCRAFT N649GT HAS BEEN APPROVED AS STRUCTURALLY ACCEPTABLE. REMOVED L - [SDR UIEA2026100900977](https://openairdocs.org/sdr/UIEA2026100900977.md): Flap · damaged · Oct 10, 2026 · N649GT · Boeing 767375 · Trailing Edge Flaps > CORROSION FOUND ON RT INBD MAIN FLAP LOWER CHORD (DAMAGE SIZE: L=12") REMOVED RT INBD MAIN FLAP LOWER CHORD AND REPLACED WITH NEW CHORD PER SRM 51-40-02. HOLE COPIED PER SRM 51-40-05. NUT-PLATES INSTALLED PER SRM 51-40-02. NO FURTHER DEFECTS NOTED. - [SDR UIEA2026100900978](https://openairdocs.org/sdr/UIEA2026100900978.md): Skin · corroded · Oct 10, 2026 · N649GT · Boeing 767375 · Leading Edge Devices > L/H WING LEADING EDGE NR 1 SLAT SKIN, FOUND DENSE CORE CORROSION (DAMAGE SIZE: L = 2.5", W=5.4") REPAIRED LT WING LEADING EDGE NR 1 SLAT SKIN IAW SRM 51-70-10 AND BMN SP1-TLS-26-0028. NO FURTHER DEFECTS NOTED. - [SDR UIEA2026072800658](https://openairdocs.org/sdr/UIEA2026072800658.md): Seal · broken · Jul 27, 2026 · N649GT · Boeing 767375 · Emergency Locator Beacon > GALLEY ELT TAMPER TAPE BROKEN. REMOVED AND REPLACED GALLEY ELT IAW AMM 25-63-03. OPS CHK OK. - [SDR UIEA2026060900455](https://openairdocs.org/sdr/UIEA2026060900455.md): Circuit Card · faulted · Jun 9, 2026 · N649GT · Boeing 767375 · Engine RPM Indicating System > RAT DEPLOYED RIGHT AFTER ROTATION ON TAKE-OFF. GREEN PRESSURE LIGHT ILLUMINATED(
REMOVED AND REPLACED LH ENG SPEED CARD & STOWED RAT PER AMM 73-21-54. NO FURTHER DEFECTS NOTED
) - [SDR UIEA2026060300430](https://openairdocs.org/sdr/UIEA2026060300430.md): Oxygen Mask · inoperative · Jun 2, 2026 · N649GT · Boeing 767375 · Crew Oxygen System > CENTER SUPERNUMERARY SEAT O2 MASK INOPERATIVE. REMOVED AND REPLACED CENTER SUPERNUMERARY O2 MASK IAW AMM 35-11-51. OPS CHECK GOOD. NO LEAKS NOTED. - [SDR UIEA2026060100424](https://openairdocs.org/sdr/UIEA2026060100424.md): Stowage Box · no test · May 30, 2026 · N649GT · Boeing 767375 · Crew Oxygen System > CAPTAIN SIDE O2 MASK AUDIO INTERCOM WILL NOT TEST. R & R CAPT SIDE O2 MASK STOWAGE IAW AMM 35-11-51 AND IPC 35-11-52-15. OPS CHECK GOOD. NO DEFECTS NOTED. - [SDR UIEA2026052600364](https://openairdocs.org/sdr/UIEA2026052600364.md): Tag · broken · May 26, 2026 · N649GT · Boeing 767375 · Standard Practices/Structures > FLIGHT DECK ELT RH DO NOT REMOVE TAG BROKEN (PORTABLE ELT)(REMOVED AND REPLACED FLIGHT DECK RH PORTABLE ELT IAW B767 AMM 25-63-03 & AIPC 25-63-52-97 AND EO 6725A129. NO FURTHER DEFECTS NOTED
) - [SDR UIEA2026051800341](https://openairdocs.org/sdr/UIEA2026051800341.md): Window · noisy · May 16, 2026 · N649GT · Boeing 767375 · Flight Compartment Windows > LOUD WHISTLING NOISES ON BOTTOM OF L1 WINDOW. PER CREW DEBRIEF, ACTUAL WINDOW IS L2 ( SLIDING WINDOW). CLEANED AND INSPECTED L2 WINDOW AERODYNAMIC ALONG WITH L1 WINDOW IAW AMM 12-16-02 AND 56-11-00 W/ NO DEFECTS NOTED. ALSO CLEANED AND INSPECTED L2 BULB SEAL - [SDR UIEA2026040500127](https://openairdocs.org/sdr/UIEA2026040500127.md): Fan · vibration · Apr 5, 2026 · N649GT · Boeing 767375 · Turbine Engine Air Inlet Section > DURING CLIMB, RIGHT ENGINE FAN VIBRATION REACHED 4.3. DURING CRUISE, VIB 0.8. PERFORMED BLADE LUBE PER AMM 72-31-02. SPINNER RE-TORQUED PER AMM 72-31-01. TRIM BALANCE AND VIBRATION SURVEY PER AMM 72-31-00. #1 BEARING CHECKS GOOD. N2 VIBE AT POWER 2.0, FAN VI - [SDR UIEA2026032700110](https://openairdocs.org/sdr/UIEA2026032700110.md): Handle · out of adjust · Mar 27, 2026 · N649GT · Boeing 767375 · Flight Compartment Windows > EMERGENCY WINDOW OUTSIDE HANDLE POPS OUT. ADJUSTED SPRING LOADED BALL LATCH OF WINDOW R2 EXTERIOR EMERGENCY ESCAPE HANDLE IAW AMM 56-11-04. OPS CHK GOOD AT THIS TIME. - [SDR UIEA2025111801297](https://openairdocs.org/sdr/UIEA2025111801297.md): Lanyard · unsecure · Nov 16, 2025 · N649GT · Boeing 767375 · Emergency Locator Beacon > ELT BY LAVATORY HAS STRING HANGING. SECURED THE ELT STRING IAW AMM 25-63-03. OPS CHECK GOOD. NO FURTHER DEFECTS NOTED. - [SDR UIEA2025102401278](https://openairdocs.org/sdr/UIEA2025102401278.md): Skin · damaged · Oct 24, 2025 · N649GT · Boeing 767375 · Nacelle/Pylon, Plate/Skin > AIRCRAFT STRUCK BY LIGHTNING. LIGHTNING STRIKE DAMAGE FOUND ON R/H INLET COWL 3:00 POSITION(PERFORMED PHASE 1 LIGHTNING STRIKE INSPECTION IAW B767 AMM 05-51. R/H ENGINE COWL DAMAGE FOUND WITHIN LIMITS IAW SRM 54-15-01-1A-1. NO FURTHER DEFECTS NOTED
) - [SDR UIEA2025100401256](https://openairdocs.org/sdr/UIEA2025100401256.md): Hf Comm · abnormal · Oct 4, 2025 · N649GT · Boeing 767375 · HF Communications System > BOTH HF COMM RADIO INOP AND SELCAL INOP(T/S WITH FIM 23-11 FT 804. RESECURED CONNECTIONS AT HF ANTENNA. OPS CHK GOOD PER AMM 23-11-00
) - [SDR UIEA2025092601246](https://openairdocs.org/sdr/UIEA2025092601246.md): Cover · detached · Sep 26, 2025 · N649GT · Boeing 767375 · Emergency Lighting > EMERGENCY EXIT LIGHT COVER FELL OFF L1 DOOR. INSTALLED EMERGENCY EXIT LIGHT COVER IAW AMM 33-51-03. NO FURTHER DEFECTS NOTED. - [SDR UIEA2025071400949](https://openairdocs.org/sdr/UIEA2025071400949.md): Bracket · damaged · Jul 14, 2025 · N649GT · Boeing 767375 · Fuselage Main, Attach Fittings > FLIGHT DECK FIRE EXTINGUISHER HOLDING BRACKET INOPERATIVE. RE-ADJUSTED FLIGHT DECK FIRE EXTINGUISHING BRACKET IAW B767 AMM 26-26-02. OPS CHECK GOOD. NO FURTHER DEFECTS NOTED AT THIS TIME. - [SDR UIEA2025062100789](https://openairdocs.org/sdr/UIEA2025062100789.md): Latch · out of adjust · Jun 19, 2025 · N649GT · Boeing 767375 · Fuselage Main, Structure > ON LANDING, FO WINDOW NR 2 EXTERNAL EMERGENCY ESCAPE HANDLE UNLATCHING. ADJUSTED FO WINDOW #2 EMERGENCY ESCAPE HANDLE LATCH & PERFORMED SYSTEM OPS CHECK OF EXTERNAL ESCAPE HANDLE IAW AMM 56-11-04. OPS CHECK GOOD AT THIS TIME. NO OTHER DEFECTS NOTED. - [SDR UIEA2025052900705](https://openairdocs.org/sdr/UIEA2025052900705.md): Skin · cracked · Jun 7, 2025 · N649GT · Boeing 767375 · Fuselage Main, Plate/Skin > SERVICE DOOR CUTOUT, AFT LOWER CORNER FUSELAGE FOUND CRACKS INDICATION, ON OPEN HOLES: #4, POSITION 8 O'CLOCK (SKIN AND BEAR STRAP) APPROX AND HOLE #5, POSITION 8 O'CLOCK (SKIN) AND 2 O'CLOCK (BEAR STRAP) APPROX.(CRACKS WERE REPAIRED PER SRM 53-10-01-2R-1 R - [SDR UIEA2025052900706](https://openairdocs.org/sdr/UIEA2025052900706.md): Bear Strap · cracked · Jun 7, 2025 · N649GT · Boeing 767375 · Fuselage Main, Plate/Skin > FORWARD ENTRY DOOR CUTOUT AFT LOWER CORNER WITH TWO CRACK INDICATIONS AT HOLE #5: 1. ON SKIN AT 3 O´CLOCK POSITION. 2. ON BEAR STRAP AT 9 O´CLOCK POSITION.(
CRACKS WERE REPAIRED PER SRM 53-10-01-2R-1 FIGURE 201 DETAIL III. NO FURTHER DEFECTS NOTED.
) - [SDR UIEA2025060300722](https://openairdocs.org/sdr/UIEA2025060300722.md): Skin · dented · Jun 7, 2025 · N649GT · Boeing 767375 · Spoilers > LH WING, SPOILER #3, LOWER SURFACE, DENT AT 10.5" FROM AFT EDGE AND 6" FROM OUTBD EDGE.(AFFECTED AREA WAS REPAIRED IN ACCORDANCE WITH B767 SRM 57-70-01-2R-1 PAG 2-5 FIG 201 SHEET 4 AND SRM 51-70-03-0G-0 PAR 5. L FIG 16. NO FURTHER DEFECTS NOTED.
) - [SDR UIEA2025060300723](https://openairdocs.org/sdr/UIEA2025060300723.md): Wedge · damaged · Jun 7, 2025 · N649GT · Boeing 767375 · Leading Edge Devices > LH WING, SLAT# 1, UPPER SIDE, WEDGE WITH HAIL DAMAGE.(LH WING, SLAT# 1, TRAILING WEDGE, UPPER SURFACE WITH DENTS (9 EAS) WERE EVALUATED AND FOUR DENTS WERE REPAIRED IAW SRM 57-43-02-2R-1 FIG.201 SHEET 2 PAG.2-3 AND SRM 51-70-10-2R-4 PAG.1,3,7 FIG-.201 SHEE - [SDR UIEA2025060300724](https://openairdocs.org/sdr/UIEA2025060300724.md): Bushing · corroded · Jun 7, 2025 · N649GT · Boeing 767375 · Engine Mount Section > FRETTING CORROSION ON BUSHING P/N BACB28X20E085 INSTALLED IN THE FWD SHEAR PIN HOLE OF THE FWD ENGINE MOUNT (P/N 311T2211-7), RH SIDE.(
BUSHING WAS REPLACED (P/N BACB28X20E085) PER DWG 311T2211-7 ID SHEET 1. NO FURTHER DEFECTS NOTED.
) - [SDR UIEA2025060300725](https://openairdocs.org/sdr/UIEA2025060300725.md): Fuel Tank · leaking · Jun 7, 2025 · N649GT · Boeing 767375 · Fuel Storage > FUEL LEAK AT CENTER TANK BETWEEN STGR L-6 AND LBL 97.5.(THE SEALANT IN THE FUEL TANK STRUCTURE WAS REPAIRED PER AMM 28-11-00-308-013. NO FURTHER DEFECTS NOTED.
) - [SDR UIEA2025060300726](https://openairdocs.org/sdr/UIEA2025060300726.md): Wedge · damaged · Jun 7, 2025 · N649GT · Boeing 767375 · Leading Edge Devices > LH WING, SLAT# 4, UPPER SIDE, WEDGE WITH HAIL DAMAGE.(LH WING, SLAT# 4, TRAILING WEDGE, UPPER SURFACE WITH DENTS (11 EAS) WERE EVALUATED AND FOUR DENTS WERE REPAIRED IAW SRM 57-43-02-2R-1 FIG.201 SHEET 2 PAG.2-3 AND SRM 51-70-10-2R-4 PAG.1,3,7 FIG.201 SHEET - [SDR UIEA2025060300728](https://openairdocs.org/sdr/UIEA2025060300728.md): Wedge · damaged · Jun 7, 2025 · N649GT · Boeing 767375 · Leading Edge Devices > LH WING, SLAT# 3, UPPER SIDE, WEDGE WITH HAIL DAMAGE.(
LH WING, SLAT# 3, TRAILING WEDGE, UPPER SURFACE WITH DENTS (7 EAS) WERE EVALUATED AND TWO DENTS WERE REPAIRED IAW SRM 57-43-02-2R-1 FIG.201 SHEET 2 PAG.2-3 AND SRM 51-70-10-2R-4 PAG.1,3,7 FIG-.201 SHEET - [SDR UIEA2025060700735](https://openairdocs.org/sdr/UIEA2025060700735.md): Skin · corroded · Jun 7, 2025 · N649GT · Boeing 767375 · Horizontal Stabilizer, Plate/Skin > RH OUTBD HORIZONTAL STABILIZER, UPPER SURFACE, AT REAR SPAR WITH CORROSION.(
RH OUTBD HORIZONTAL STABILIZER, UPPER SURFACE, AT REAR SPAR WITH CORROSION LEVEL 2 WAS REPAIRED IAW CMA-TLS-25-0045. NO FURTHER DEFECTS NOTED.
) - [SDR UIEA2025060700736](https://openairdocs.org/sdr/UIEA2025060700736.md): Skin · corroded · Jun 7, 2025 · N649GT · Boeing 767375 · Horizontal Stabilizer, Plate/Skin > RH OUTBD HORIZONTAL STABILIZER, UPPER SURFACE, AT FRONT SPAR FROM STA 0.0 TO STA 107.927, CORROSION AROUND FASTENERS. L= 6.0 IN W=1.5 IN.(RH OUTBD HORIZONTAL STABILIZER, UPPER SURFACE, AT FRONT SPAR FROM STA 0.0 TO STA 107.927, CORROSION LEVEL 2 AROUND FAST - [SDR UIEA2025031700353](https://openairdocs.org/sdr/UIEA2025031700353.md): Evas Unit · inoperative · Mar 17, 2025 · N649GT · Boeing 767375 · Emergency Equipment > DURING EVAS OPS CHECK, FOUND CAPTAINS EVAS INOP (BLOWER INOP)(
REMOVED & REPLACED EVAS CAPTAINS SIDE AS PER B-767-300 AMM 25-60-99. OPS CHECK GOOD.
) - [SDR UIEA2025031200260](https://openairdocs.org/sdr/UIEA2025031200260.md): Skin · no discrepancy · Mar 12, 2025 · N649GT · Boeing 767375 · Standard Practices/Structures > LIGHTNING STRIKE AT 17000 FT. SUSPECT STRIKE IMPACT ON CAPTAIN'S SIDE IN THE VICINITY OF THE NOSE.(PERFORMED LIGHTNING STRIKE DAMAGE PHASE INSPECTION IAW B767 AMM 05-51-19. FOUND LIGHTNING IMPACT AND POSSIBLE EXIT POINT AT 2 TO 3 O'CLOCK POSITION BETWEEN ST - [SDR UIEA2025021200132](https://openairdocs.org/sdr/UIEA2025021200132.md): Wire Harness · damaged · Feb 12, 2025 · N649GT · Boeing 767375 · APU System Wiring > AIR TURN BACK DUE TO APU SHUTDOWN IN FLIGHT. LEFT GENERATOR ON MEL SO APU IS REQUIRED. APU RESTARTED ON 3RD ATTEMPT.(
PER ENGINEERING AND MANAGEMENT REQUEST, R/R APU HARNESS WIRE PN: W020-212R-24 IAW WDM 49-14-11-1 AND SWPM 20-25-00 AND SWPM 20-60-00. DUE TO - [SDR UIEA2024122901187](https://openairdocs.org/sdr/UIEA2024122901187.md): Transcowl · damaged · Dec 30, 2024 · N649GT · Boeing 767375 · Engine Thrust Reverser > LH ENG T/REV WIRE MESH DAMAGED AT 0700 O'CLOCK POSITION. C/W EO 6778A019 REV 5 PART 1 INTERIM REPAIR. C/W PART 2 PERMANENT REPAIR AT NEXT A-CHECK.(
REMOVED TRANSLATING COWL FROM L/H THRUST REVERSER OUTBOARD HALF IAW AMM 78-31-10. OK TO INSTALL TRANSLATING CO - [SDR UIEA2024122901188](https://openairdocs.org/sdr/UIEA2024122901188.md): Radome · eroded · Dec 30, 2024 · N649GT · Boeing 767375 · Aerodynamic Fairings > FWD FUSELAGE RADOME SURFACE, FOUND SEVERAL AREAS OF EROSION.(
INSPECTED SURFACE DEFECT AT NOSE RADOME. FOUND EVIDENCE OF PEELING PAINT IAW B767 AMM 53-12-01 CLEANED AND PAINTED AREA IAW B767 AMM 53-12-01
) - [SDR UIEA2024122901189](https://openairdocs.org/sdr/UIEA2024122901189.md): Oxygen Mask · contaminated · Dec 30, 2024 · N649GT · Boeing 767375 · Passenger Oxygen System > LAV PORTABLE OXYGEN MASK CONTAMINATED.(REMOVED AND REPLACED LAV PORTABLE OXYGEN MASK AS REQUIRED PER 767 AMM 35-31-01. OPS CHK GOOD.
) - [SDR UIEA2024122901190](https://openairdocs.org/sdr/UIEA2024122901190.md): Panel · loose · Dec 30, 2024 · N649GT · Boeing 767375 · Nacelle/Pylon, Main Frame > #2 ENGINE I/B CORECOWL HINGES DAMAGED, DIFFICULT TO OPEN AND CLOSE. REQUIRES EVALUATION.(EVALUATED AND FOUND SKIRT PANEL WITH LOOSE AND MISSING FASTENERS. LOCATED AND INSTALLED NEW FASTENERS IAW SRM 51-40-02-06. OPS CHECK GOOD.
) - [SDR UIEA2024122901191](https://openairdocs.org/sdr/UIEA2024122901191.md): Cdu · inoperative · Dec 30, 2024 · N649GT · Boeing 767375 · Engine Thrust Reverser > LEFT T/R INOP.(REMOVED CENTER DRIVE UNIT AT LEFT ENGINE INBOARD SIDE AS PER REF B747 AMM 78-31-21. OK TO INSTALL. INSTALLED CENTER DRIVE UNIT AT LEFT ENGINE INBOARD SIDE AS PER REF B747 AMM 78-31-21. OPS CHECK GOOD.
) - [SDR UIEA2024120301158](https://openairdocs.org/sdr/UIEA2024120301158.md): Switch · faulted · Dec 3, 2024 · N649GT · Boeing 767375 · Stabilizer Position Indicating > UNSCHEDULED STAB TRIM MSG ON DECENT. CLEARED SHORTLY AFTER.(R/R STAB TRIM LIMIT SWITCH MODULE ASSY IAW AMM 27-48-01. OPS CHECK GOOD NO DEFECTS NOTED. PERFORMED MCDP GROUND TEST 40, 65 AND 66. ALL TEST GOOD, NO DEFECTS NOTED. PARTS EFECTIVE PER IPC 27-48-01- - [SDR UIEA2024111301085](https://openairdocs.org/sdr/UIEA2024111301085.md): Elt · inoperative · Nov 12, 2024 · N649GT · Boeing 767 · Emergency Equipment > REF W/O 138840, DURING OPS CHECK OF FIXED ELT FOUND TO BE INOPERATIVE.(
R/R FIXED ELT PER EO OT-23-0084. OPS CHECK GOOD. DMI 220446 CLOSED
) - [SDR UIEA2024082300843](https://openairdocs.org/sdr/UIEA2024082300843.md): Skin · damaged · Aug 23, 2024 · N649GT · Boeing 767375 · Ailerons > RH OTBD AILERON TRAILING EDGE LIGHTNING STRIKE(TRANSFER TO NON-MEL DMI 215328 DUE DATE 27AUG24.
/LP 1872886 M1: C/W PART 3 PERMANENT REPAIR PER ATLAS EA 6757A156- CS REV 0. NON-MEL DMI 215328 CLOSED - [SDR UIEA2024080200776](https://openairdocs.org/sdr/UIEA2024080200776.md): Indication Sys · faulted · Aug 2, 2024 · N649GT · Boeing 767375 · Crew Oxygen System > AFTER LANDING O2 BOTTLE INDICATES 40 PSI. CONFIRMED EICAS IND INOP. REF DMI 213995 PER MEL 35-11-02-01 CAT B DUE DATE 8AUG24. MMP PERFORMED. BOTTLE #1 1400 PSI, BOTTLE #2 1300 PSI, AVERAGE 1600 PSI. R/R VOLT AVG UNIT PER AMM 35-11-06. OPS CHECK GOOD. - [SDR UIEA2024072600753](https://openairdocs.org/sdr/UIEA2024072600753.md): Averaging Unit · faulted · Jul 26, 2024 · N649GT · Boeing 767375 · Oxygen System > ON GROUND OXYGEN PRESSURE SHOWS 40 PSI.(
R/R AVERAGING UNIT IAW AMM 35-11-06. OPS & LEAK CHECK GOOD. DMI 213524 CLOSED.
) - [SDR UIEA2024040800267](https://openairdocs.org/sdr/UIEA2024040800267.md): Shroud · damaged · Apr 7, 2024 · N649GT · Boeing 767375 · Emergency Equipment > L1 DOOR EMERGENCY ESCAPE ROPE SHROUD DAMAGED.(PERFORMED TIME LIMITED REPAIR ON L1 DOOR ESCAPE ROPE RETAINER SHROUD IAW EA 6725A0025. TRANSFER TO NON-MEL DMI 206255 & 206256 DUE DATE 8APR2024. LP 1807206 M2: R/R SHROUD IAW AMM 52-09-01. NO FURTHER DEFECTS NO - [SDR UIEA2024021700090](https://openairdocs.org/sdr/UIEA2024021700090.md): Elt · unknown · Feb 17, 2024 · N649GT · Boeing 767375 · Emergency Locator Beacon > DURING OPS CHECK OF FIXED ELT PER W/C # A-23--339-01(
TRANSFERRED TO MDDR 203168 PER DDG 25-63-10-02C CAT D DUE 16JUM24. MX ACTIONS C/W, PLACARDS INSTALLED. PRFORMED ELT OPS CHECK PER CAD A-23-999-01, TEST NORMAL. THIS CLEARS DMI 203168, PLACARD REMOVED.
MAIN CARGO DOOR SHOWS OPEN DURING CRUISE. INDICATION WENT OUT DURING DESCENT AT FL 340. "MAIN CARGO DOOR" EICAS MSG.(FOUND MAIN CARGO DOOR LOCKED WARNING SENSOR S892 OUT OF TOLERANCE. RESHIMMED & ADJUSTMENTED SENSOR TO WITHIN LIMITS, DOOR OPS CHECK NORMAL I - [SDR UIEA2023122201010](https://openairdocs.org/sdr/UIEA2023122201010.md): Computer · unknown · Dec 22, 2023 · N649GT · Boeing 767375 · Auto Flight System > RETURN TO BLOCK AFTER LOW SPEED RTO DUE MASTER CAUTION LIGHT AND BEEPER. "AUTOTHROTTLE DISCONNECT" EICAS MSG. SPED WAS AROUND 40KTS.(
DEFERRED IAW MEL 22-30-01 DMI 199674 CONDITION INSP IAW AMM 05-51-14 NOT REQUIRED AS RTO WAS BELOW 40 KNOTS.R/R TMC COMPUTER Next page: https://openairdocs.org/aircraft/N649GT/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 = 'N649GT' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N649GT/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.