# Service difficulty reports: N1997A A list on [N1997A](https://openairdocs.org/aircraft/N1997A.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. Page 1 of 8 · 374 reports - [SDR ABXR2026060400010](https://openairdocs.org/sdr/ABXR2026060400010.md): Angle · cracked · Jun 4, 2026 · N1997A · Boeing 76733A · Wing, Attach Fittings > RIGHT WING L/E #9 SLAT AREA INTERNAL ANGLE CRACKED AT LOWER FWD WEB LOWER ANGLE. LES668. FABRICATED NEW ANGLE IAW B767 SRM 57-41-13 REPAIR 1 - [SDR ABXR2026060400009](https://openairdocs.org/sdr/ABXR2026060400009.md): Frame · corroded · Jun 4, 2026 · N1997A · Boeing 76733A · Fuselage Main, Frame > CORROSION AT STA. 1219 RBL22 "J" FRAME FOUND TO BE OUT OF LIMITS IAW B767 SRM 53-00-511. - [SDR 21GA202509030017](https://openairdocs.org/sdr/21GA202509030017.md): Controller · faulted · Aug 29, 2025 · N1997A · Boeing 76733A · Fire Detection > ON APPROACH, RECEIVED WHEEL WELL FIRE EICAS MESSAGE. DECLARED EMERGENCY AND LANDED WITHOUT INCIDENT. INSPECTED AND FOUND NO EVIDENCE OF FIRE. REPLACED DETECTION CONTROL CARD. - [SDR 21GA20250610011](https://openairdocs.org/sdr/21GA20250610011.md): Battery · inoperative · Jun 10, 2025 · N1997A · Boeing 76733A · Emergency Lighting > DURING SERVICE CHECK, L1 DOOR EMERGENCY LIGHT FAILED TO ILLUMINATE. REPLACED BATTERY ASSEMBLY. - [SDR UIEA2024112901131](https://openairdocs.org/sdr/UIEA2024112901131.md): Pseu · malfunctioned · Nov 29, 2024 · N1997A · Boeing 76733A · Wing, Control Surfaces > AS FLAPS MOVED FROM 1 TO UP ON CLIMB OUT; FLAP (RED). EICAS STATUS MSG: NOSE A/G DISAGREE ALSO F/O HAD SPEED LIM ON HIS SPEED TAPE(

TROUBLESHOT & FOUND PSEU CARD MSG 002 AND TARGET MSG 266, TARGET MSG 266, FOUND RH MSG 002, SENSOR HARNESS 266, R/R PER AMM 3 - [SDR UIEA2024112701117](https://openairdocs.org/sdr/UIEA2024112701117.md): Wedge · damaged · Nov 27, 2024 · N1997A · Boeing 76733A · Leading Edge Devices > 8028 - EA-1957A155 PART(3) REV(0) WINGS - LEADING EDGE DEVICES - RH WING #8 LEADING EDGE SLAT (PN 114T4105-58 /SN 000598) TRAILING EDGE WEDGE EXISTING REPAIR DELAMINATION - TIME LIMITED REPAIR(

PERMANENT REPAIR WAS PERFORMED IAW EA 1957A155. NO FURTHER DEFEC - [SDR UIEA2024112601116](https://openairdocs.org/sdr/UIEA2024112601116.md): Bear Strap · cracked · Nov 27, 2024 · N1997A · Boeing 76733A · Fuselage Main, Plate/Skin > LH FWD DOOR, AFT LOWER CORNER WITH CRACK INDICATION AT SECOND LOWER HOLE ON BEAR STRAP APPROX. 10 O'CLOCK.(

CRACK WAS REPAIRED IAW EA 6753A937. NO FURTHER DEFECTS NOTED

) - [SDR UIEA2024112601115](https://openairdocs.org/sdr/UIEA2024112601115.md): Shear Tie · corroded · Nov 27, 2024 · N1997A · Boeing 76733A · Fuselage Internal Mounting Structure > BULK CARGO COMPARTMENT, STA 1480 BTW STGR 28R-29R FRAME WITH CORROSION(

SHEAR TIE WAS REPLACED IAW DWG 146T1519. NO FURTHER DEFECTS NOTED

) - [SDR UIEA2024112501114](https://openairdocs.org/sdr/UIEA2024112501114.md): Skin · scratched · Nov 27, 2024 · N1997A · Boeing 76733A · Fuselage Main, Plate/Skin > TRAFFIC ALERT & COLLISION AVOIDANCE SYS HEALTH CHECK, ON TCAS UPPER ANTENNA WITH SCRATCHES ON FUSELAGE SKIN(

THE TCAS UPPER ANTENNA DOUBLER WAS BLEND OUT AND INSPECTION WERE PERFORMED IAW TRE 6753708. NO FURTHER DEFECTS NOTED.

) - [SDR UIEA2024112501113](https://openairdocs.org/sdr/UIEA2024112501113.md): Web · corroded · Nov 27, 2024 · N1997A · Boeing 76733A · Fuselage Miscellaneous Structure > AFT CARGO, BTW STA 1263 AND DOOR FRAME, BTW STRG 32R AND 32R, CORROSION ON WEB.(

CLIP P/N 146T8081-13 SMALL AUTHORIZATION IAW CONSECUTIVE NUMBER M675498 & SRM 51-40-02-0G-0. NO FURTHER DEFECTS NOTED.CORROSION REMOVED

) - [SDR UIEA2024112401111](https://openairdocs.org/sdr/UIEA2024112401111.md): Frame · corroded · Nov 27, 2024 · N1997A · Boeing 76733A · Fuselage Main, Frame > FRAME AT STA 1480 BETWEEN STGR 27R / 29R WITH CORROSION (BULK CARGO COMPARTMENT AREA)(

FRAME N/P 146T1519-3 WAS MANUFACTURED IN ACCORDANCE SMAL AUTHORIZATION BY BOEING MESSAGE CMA-TLS-24-0222-01B (MXA ENGINEERING TASK CARD M6753499 ISSUED DATE NOVEMBER 19, 2 - [SDR UIEA2024112201104](https://openairdocs.org/sdr/UIEA2024112201104.md): Shear Tie · corroded · Nov 27, 2024 · N1997A · Boeing 76733A · Fuselage Internal Mounting Structure > BULK CARGO, FLOOR LEVEL AT FRAME 1540, SHEAR TIE WITH CORROSION BTW STRG 39R AND 38R.(

THE SHEAR TIE WITH CORROSION WAS REMOVED. THE AREA WAS CLEANED. THE NEW SHEAR TIE WAS DRILLED AND INSTALLED CORRECTLY IAW SRM 51-40-02-0G-0. NO FURTHER DEFECTS NOTED

) - [SDR UIEA2024112201103](https://openairdocs.org/sdr/UIEA2024112201103.md): Skin · cracked · Nov 27, 2024 · N1997A · Boeing 76733A · Service Doors > RH FWD DOOR, AFT LOWER CORNER WITH CRACK INDICATION AT THIRD HOLE ON SKIN APPROX 1 O'CLOCK, AND VISUAL CRACK (CONFIRMED WITH HFEC) AT FOURTH HOLE ON SKIN AND BEAR STRAP APPROX. 2 O'CLOCK AND CONTINUE TO APPROX 7 O'CLOCK.
(

IT WAS REPAIRED IAW EA 6753A937 - [SDR UIEA2024112201102](https://openairdocs.org/sdr/UIEA2024112201102.md): Support Beam · corroded · Nov 27, 2024 · N1997A · Boeing 76733A · Fuselage Main, Structure > BULK CARGO DOOR, INTERNAL STRUCTURE, CORROSION BTW BEAMS 2 AND 4.(

THE AREA WAS CLEANED, NEW SUPPORT WAS DRILLED, SUPPORT BEAM WAS INSTALLED. THE BEAM SUPPORT WAS REPLACED IAW SRM 51-10-02-0G-0. NO FURTHER DEFECTS NOTED

) - [SDR UIEA2024112201101](https://openairdocs.org/sdr/UIEA2024112201101.md): Bearing · coked · Nov 27, 2024 · N1997A · Boeing 76733A · Turbine Section > ENGINE 1, BEARING #5, LH/RH SUMP PIPES WITH LEAK EVIDENCE.(

DURING VISUAL EXAMINATION, OIL COKE BUILD-UP WAS FOUND, COKING WAS REMOVED AND NO OIL LEAK WAS FOUND IN LH/RH SUMP PIPES IAW AMM SUBTASK 72- 50-00-216-032-H00 REV. 143 DATE: 22 AUG 2024. C/W IDLE LE - [SDR UIEA2024112201100](https://openairdocs.org/sdr/UIEA2024112201100.md): Splice · corroded · Nov 27, 2024 · N1997A · Boeing 76733A · Fuselage Miscellaneous Structure > BULK CARGO COMPARTMENT AT STA 1502 BTW STGR 31R-32R SPLICE WITH CORROSION.(

A NEW SPLICE WEB WAS MANUFACTURED AND INSTALLED IAW SRM 51-10-02-0G-0. NO FURTHER DEFECTS NOTED.

) - [SDR UIEA2024112201099](https://openairdocs.org/sdr/UIEA2024112201099.md): Skate Angle · cracked · Nov 27, 2024 · N1997A · Boeing 76733A · Nacelle/Pylon, Main Frame > CRACK ON LH SKATE ANGLE ON STRUT #2 (FOUND DURING SEALANT REMOVAL)(

A SEGMENT OF THE SKATE WITH CRACK WAS REMOVED, AND THE NEW SEGMENT WAS MANUFACTURED AND INSTALLED IAW FVCI CONTROL EO 24190-2. NO FURTHER DEFECTS NOTED.

) - [SDR UIEA2024112201098](https://openairdocs.org/sdr/UIEA2024112201098.md): Frame · corroded · Nov 27, 2024 · N1997A · Boeing 76733A · Fuselage Main, Frame > BULK CARGO COMPARTMENT AT STA 1480 BTW STGR 31R-32R FRAME WITH CORROSION(

FRAME WAS MANUFACTURED AND REPLACED WITH THE NEW ONE. NO FURTHER DEFECTS NOTED

) - [SDR UIEA2024111901096](https://openairdocs.org/sdr/UIEA2024111901096.md): Skin · debonded · Nov 27, 2024 · N1997A · Boeing 76733A · Ailerons > RH WING, INBOARD AILERON, LEADING EDGE DISBONDED BTW RIB 1 AND 2.(

RH WING, INBOARD AILERON, L/E BETWEEN RIB 1 AND 2 WAS REPAIRED AS PER B767-300 SRM 57-60-01-2R-1 FIG. 201, SHEET 4, PAG. 1-10 AND B767-300 SRM 51-70-17-0G-0 PAR. 4G, FIG. 15, PAG. 16, 17,42. - [SDR UIEA2024051900395](https://openairdocs.org/sdr/UIEA2024051900395.md): Light · broken · May 19, 2024 · N1997A · Boeing 76733A · Emergency Lighting > EMERGENCY EXIT LIGHT BY L1 BOOR BROKEN(

RESECURED EMERGRNCY EXIT SIGN LENSE IAW 33-51-01. NO FURTHER DEFECTS NOTED

) - [SDR UIEA2023071300756](https://openairdocs.org/sdr/UIEA2023071300756.md): Hose · unknown · Jul 13, 2023 · N1997A · Boeing 76733A · Crew Oxygen System > O2 DISCHARGED COMPLETELY THROUGH FO'S REGULATOR IN MASSIVE AND SUDDEN LEAK(

FOUND FO'S OXYGEN MASK BOX CONNECTION HOSE BLOWN OFF AND MASSIVELY LEAKING. REMOVED AND REPLACED CONNECTION HOSE ASSY IAW AMM 20-11-00, OPS AND LEAK CHECHED GOOD IAW AMM 35-11-00. RH PIMU FAULT MESSAGE.(

R/R RH PIMU & OPS CHECK OK PER AMM 77-35-02.

) - [SDR UIEA2023040300309](https://openairdocs.org/sdr/UIEA2023040300309.md): Lead · unknown · Apr 3, 2023 · N1997A · Boeing 76733A · Airborne Auxiliary Power Unit (APU) System > ENG #1 LOWER HIGH TENSION LEAD DAMAGED.(

REMOVED & REPLACED ENG #1 LOWER HIGH TENSION LEAD IAW 767-300 AMM 74-21-02. PERFORMED AUDIBLE TEST FOR ENG #1, AUDIBLE TEST OK IAW AMM 74-00-00

) - [SDR UIEA2023040300308](https://openairdocs.org/sdr/UIEA2023040300308.md): Unknown · unknown · Apr 3, 2023 · N1997A · Boeing 76733A · Oxygen System > FWD E/E CREW OXYGEN NEED SERVICE TO FULL.(

SERVICED FWD E&E CREW OXYGEN AS PER B767 AMM CH 12-15-08, AC 43.18-1B PAR 9-46 THRU 9-51 PGS 9-448 THRU 9-455. OPS CHECK GOOD. NO LEAKS FOUND.

/

PN: 801307-00 SN ST298851 DUE DATE 31 JUL 25 MFG DATE 31 JAN 1 - [SDR UIEA2023040300307](https://openairdocs.org/sdr/UIEA2023040300307.md): Controller · unknown · Apr 3, 2023 · N1997A · Boeing 76733A · Pneumatic System > CABIN COMPT TEMP CONTROL SYS INOP.(

R/R CABIN COMPT TEMP CONTROLLER M195 & ZONE TEMP CONTR. 1 SYS. OPS TEST GOOD PER AMM 21-61-03. MDDR 182947 CLEARED UP

) - [SDR UIEA2023040300306](https://openairdocs.org/sdr/UIEA2023040300306.md): Unknown · unknown · Apr 3, 2023 · N1997A · Boeing 76733A · Airborne Auxiliary Power Unit (APU) System > ECM 2023P-168 N1997A ENG #1 ESN #702928 IS EXPERIENCING HIGH FAN VIBRATION. A TRIM BALANCE IS REQUIRED TSLV 10,240 CSLV 3,348.(

PERFORMED LH ENG RUN UP PER AMM 71-00-00. INCREASED N2 POWER TO 99% & FAN VIB DID NOT EXCEED 0.9. NO DISCREPANCY NOTED. OPS CHECK - [SDR UIEA2022122701217](https://openairdocs.org/sdr/UIEA2022122701217.md): Lamp · inoperative · Dec 23, 2022 · N1997A · Boeing 76733A · Emergency Lighting > EMERGENCY LIGHT AT L1 DOOR INOPERATIVE. REPLACED THE LAMPS, OPS CHECKED NORMAL IAW AMM 33-51-00. - [SDR UIEA2022053100562](https://openairdocs.org/sdr/UIEA2022053100562.md): Pca · leaking · May 26, 2022 · N1997A · Boeing 76733A · Aileron Tab Control System > WITH LEFT AND CENTER HYD SYS DEPRESSURIZED LEFT INBOARD AILERON FLOATS UP DURING LEVEL FLIGHT RESULTING IN HARD LEFT ROLL. FOUND LEFT INBOARD AILERON INBOARD & OUTBOARD PCA'S LEAKING AT SCRAPPER SEALS. REMOVED AND REPLACED O/B PCA IAW B767 AMM 27-11-48. STEPS - [SDR UIEA2022053100561](https://openairdocs.org/sdr/UIEA2022053100561.md): Pca · erratic · May 25, 2022 · N1997A · Boeing 76733A · Aileron Tab Control System > AIRPLANE WAS HAVING PROBLEMS MAINTAINING VNAV PTH ON THE ARRIVAL ROUTE. AFTER DISCONNECTING AUTOPILOT I FELT HEAVY RESISTANCE WITH AILERON FLIGHT CONTROLS. BOTH LEFT AND RIGHT AILERON INPUT AT AIRSPEEDS ABOVE 200 KTS. AILERON TRIM SHOWED ZERO WITH LEVEL CONTRO - [SDR UIEA2022042000350](https://openairdocs.org/sdr/UIEA2022042000350.md): Transducer · none · Apr 19, 2022 · N1997A · Boeing 767 · Oxygen System > SUPERNUMERARY O2 INDICATION IS ERRATIC(

TRANSFERRED TO MMDR 164289 IAW MEL 35-11-03-02A, CAT C.

/

LOGPAGE 1504123 - ITEM #4: REMOVED AND REPLACED PAX O2 TRANSDUCER PER AMM 35-11-04. THIS CLEARS MDDR 164289.

) - [SDR UIEA2022032800249](https://openairdocs.org/sdr/UIEA2022032800249.md): None · none · Apr 16, 2022 · N1997A · Boeing 767 · Cargo Compartments > CORROSION IN THE AFT CARGO COMPARTMENT HORIZONTAL ATTACH FITTING BETWEEN STR,23R AND STR.24R JUST AFT OF THE BS.1065 BULKHEAD. DOT 129-097(

REMOVED AND REPLACE THE RH HORIZ. FITTING, 2EA. ATTACH BRACKETS AND 1 EA. WEB AT STA. 1065-1109 STR. 23R-24R IAW - [SDR UIEA2022040800268](https://openairdocs.org/sdr/UIEA2022040800268.md): None · none · Apr 16, 2022 · N1997A · Boeing 767 · Cargo Compartments > CORROSION AROUND FASTENER HOLE AND UNDER ROLLER TRAY IN THE AFT CARGO COMPARTMENT FLOOR BEAM UPPER CHORD LOWER SURFACE BS.1241 LBL.43.(

REMOVED, FABRICATED NEW, AND INSTALLED NEW AFT CARGO COMPARTMENT FLOOR BEAM UPPER CHORD AT STA 1241 IAW B767 SRM 53- - [SDR UIEA2022040800270](https://openairdocs.org/sdr/UIEA2022040800270.md): Fitting · none · Apr 16, 2022 · N1997A · Boeing 767 · Cargo Compartments > CORROSION IN THE AFT CARGO COMPARTMENT HORIZONTAL ATTACH FITTING BETWEEN STR,23L AND STR.24L JUST AFT OF THE BS.1065 BULKHEAD(

REMOVED AND REPLACED THE LH HORIZ. FITTING AT STA 1065-1109 STR. 23L-24L IAW B767 SRM 51-40-02. (CORROSION LEVEL 2)

) - [SDR UIEA2022041000279](https://openairdocs.org/sdr/UIEA2022041000279.md): Fitting · none · Apr 16, 2022 · N1997A · Boeing 767 · Nacelle/Pylon Structure > RH PYLON OB SIDE AFT STA 280 APPROX LWR FITTING CRACKED AT LWR END.(

REMOVED AND REPLACED RH PYLON OB SIDE AFT LWR FITTING STA 280 IAW B767 SRM 51-40-02, 51-40-05.

) - [SDR UIEA2022041400306](https://openairdocs.org/sdr/UIEA2022041400306.md): None · none · Apr 16, 2022 · N1997A · Boeing 767 · Wing Structure > RH WING UPPER SIDE BODY SPLICE CENTER WING WBL.95 BTWN. 1, 2 STRINGERS U 10, U7 SKIN FOUND CORRODED AREA DOT 11/ 0013(

REMOVED CORROSION FROM RH WING UPPER SIDE BODY SPLICE CENTER WING WBL.95 BTWN. 1, 2 STRINGERS U 10, U7 SKIN. ORIGINAL MATERIAL.200" REMAIN - [SDR UIEA2022041800312](https://openairdocs.org/sdr/UIEA2022041800312.md): Bottle · low pressure · Apr 16, 2022 · N1997A · Boeing 76733A · Crew Oxygen System > CREW O2 LOW AT DEPARTURE CREW O2 READ 1600 ON ARRIVAL 1220(

REMOVED AND REPLACED CREW O2 BOTTLE IAW AMM 12-15-08 & LEAKED CHECKED OKAY PER GMM 3.25.3. NO DEFECTS NOTED AT THIS TIME.

) - [SDR UIEA2022012300073](https://openairdocs.org/sdr/UIEA2022012300073.md): None · none · Jan 23, 2022 · N1997A · Boeing 76733A · Landing Gear Retraction/Extension System > GEAR DISAGREE EICAS AFTER SELECTING GEAR DOWN. RAN QRH PROCEDURES(

ON WALK AROUND FOUND TAIL SKID RETRACTED. PERFORMED FIM 32-30 FT 305. ON PSEU BITE TEST FOUND MSG '248' TAIL SKID RETRACT. PERFORMED TAIL SKID EXTEND OPS TEST PER AMM 32-71-00-715-001 OPS GOO - [SDR UIEA2022010500006](https://openairdocs.org/sdr/UIEA2022010500006.md): Switch · none · Jan 5, 2022 · N1997A · Boeing 76733A · Lighting System > EMERGENCY LIGHT KORRY SWITCH INOP(

REMOVED AND REPLACED EMERGENCY LIGHT KORRY SWITCH IAW AMM 33-13-00. OPS TEST GOOD.

) - [SDR UIEA2021120502445](https://openairdocs.org/sdr/UIEA2021120502445.md): Elevator System · failed · Dec 6, 2021 · N1997A · Boeing 76733A · Elevator Control System > ELEVATOR NOT RETURNING TO CENTER POSITION WHEN DOING FLIGHT CONTROL CHECK.(

PERFORMED ELEVATOR POSITION INDICATING SYSTEM OPS TEST IAW AMM 27-38-00. OPS CHECK GOOD AT THIS TIME. AC OK FOR SERVICE.

) - [SDR UIEA2021110802362](https://openairdocs.org/sdr/UIEA2021110802362.md): None · none · Nov 6, 2021 · N1997A · Boeing 76733A · Air Conditioning System > FWD EQPT VAL EICAS MSG MOMENTARILY APPEARED DURING ROTATION. REPEAT WRITE UP.(

REF ITEM M9 LP 1431441 FOR CORRECTIVE ACTION. EQ COOLING GROUND VALVE POSITION FROM N2 SPEED CARD PER AMM 21-58-00. PERFORMED VALVE OPERATIONAL CHECK IAW AMM 21-58-00 VALVE HEALTH - [SDR UIEA2021110802365](https://openairdocs.org/sdr/UIEA2021110802365.md): None · none · Nov 6, 2021 · N1997A · Boeing 76733A · Fuel Control/Turbine Engines > L ENG SPEED CARD EICAS MSG.(

FOUND CANNON PLUG D4978P WITH BROKEN WIRE PIN 38 TO N2 SPEED CARD. RETERMINATED IAW SWPM 70-60-02 AND WDM77-12-12. PERFORMED IDLE RUN IAW AMM 7100-00 ALL OPS CHECK GOOD.

) - [SDR UIEA2021110502349](https://openairdocs.org/sdr/UIEA2021110502349.md): None · none · Nov 5, 2021 · N1997A · Boeing 76733A · Directional Gyro and Indicating System > DURING TAXI OUT CAPTS PFD & UPPER EICAS SCREENS WENT BLANK.(

CAPT'S ADI AND UPPER EICAS CAME BACK AFTER SHUTDOWN. SUPPLIED AIR FOR HOT/HUMID WEATHER CONDITIONS IAW B767AMM 21-00-00-862-068.

) - [SDR UIEA2021110802370](https://openairdocs.org/sdr/UIEA2021110802370.md): None · none · Nov 5, 2021 · N1997A · Boeing 76733A · Fuel Control/Turbine Engines > L ENG SPEED CARD STATUS MSG REPEAT WRITE UP.(

R/R N2 SPEED CARD ON L/H ENG. FAULT CLEARED. FOUND CONNECTOR ON D10064 TO HAVE DAMAGED THREADED INSERTS CAUSING SPEED CARD NOT TO STAY SECURED. SEE LP 1440560 ITEM 6 FOR CORRECTION REF B767 73-21-54. N2 SPEED CAR - [SDR UIEA2021110502351](https://openairdocs.org/sdr/UIEA2021110502351.md): None · none · Nov 5, 2021 · N1997A · Boeing 76733A · Fuel Control/Turbine Engines > REPEAT WRITE UP LEFT ENG SPEED CARD STATUS MESSAGE AFTER ENG START(

PERFORMED ENG N2 SPEED CARD TEST AS PER B767 AMM TASK 73-21-54-705-005-H00 TEST OK.

) - [SDR UIEA2021110402347](https://openairdocs.org/sdr/UIEA2021110402347.md): None · none · Nov 4, 2021 · N1997A · Boeing 76733A · Fuel Control/Turbine Engines > L ENG SPEED CARD STATUS MESSAGE AFTER START...REPEAT WRITE UP(

PERFORMED FIM 73-21 TASK TT#871 BLOCK #21 FOUND L END SPEED CARD DISPLAYED. REMOVED/REPLACED M1083 N2 SPEED CARD, PERFORMED ADJUSTMENT/TEST IAW AMM 73-21-54-705-005-H00, MESSAGE CLEARED OPS TEST - [SDR UIEA2021110402344](https://openairdocs.org/sdr/UIEA2021110402344.md): None · none · Nov 4, 2021 · N1997A · Boeing 76733A · Fuel Control/Turbine Engines > L. ENG SPEED CARD STATUS MESSAGE AFTER START(

T/S PER B767 AMM 73-21-54-705-005-HOO AND B767 FIM 73-21 FAULT TREE 871. TEST PASSED NORMAL. MESSAGE CLEARED. COULD NOT DUPLICATE ON GROUND AT THIS TIME. MCC ADVISED

) - [SDR UIEA2021110302331](https://openairdocs.org/sdr/UIEA2021110302331.md): None · none · Nov 2, 2021 · N1997A · Boeing 76733A · Engine Ignition Analyzer > LEFT / #1 ENGINE "VIB" INDICATION BETWEEN 1 AND 4 ON STATUS PAGE DURING DEPARTURE. FLUCTUATIONS WERE ALSO SLIGHTLY FELT.(

RAN #1 ENGINE HIGH POWER RUN VIBRATION SURVEY PER B767 AMM 71-00-00-735-370-H03. AT IDLE. VIBE 0.7, EGT 319, FF 1.3 AT MAX POWER SETTING - [SDR UIEA2021100202163](https://openairdocs.org/sdr/UIEA2021100202163.md): Radome · damaged · Sep 30, 2021 · N1997A · Boeing 76733A · Fuselage Main, Bulkhead > BIRD STRIKE ON RADOME. INSPECTED NOSE RADOME FOUND DAMAGE ON THE EXTERNAL SIDE SURFACE WAS OUT OF LIMITS IAW AMM 05-51-18 & SRM 53-10-72.LP 1401419, ITEM M6: REMOVED AND REPLACED NOSE RADOME IAW AMM 53-12-01, ADJUSTED AND SAFETIED NOSE RADOME IAW AMM 53-12-01- - [SDR UIEA2021082501877](https://openairdocs.org/sdr/UIEA2021082501877.md): Valve · faulted · Aug 24, 2021 · N1997A · Boeing 76733A · APU Bleed Air System > APU PNEUMATICS INOP ( AUXILIARY POWER UNIT, PNEUMATIC FUNCTION)(

TRANSCRIBED TO MEL LIST MDDR 152437 DMI # 49-11-01-01 DUE 03SEP21, CAT C. MAINT ACTIONS C/W PER 152437. PLACARDS APPLIED.

/

25AUG21 - 1397821 - ITEM# 5 - CVG - REMOVED FLOW SENSING MODU - [SDR UIEA2021082401862](https://openairdocs.org/sdr/UIEA2021082401862.md): Control Valve · faulted · Aug 23, 2021 · N1997A · Boeing 76733A · Cabin Temperature Control System > AFT CABIN COMPARTMENT SHOWS 7D EVENT THOUGH AFT CABIN TEMPERATURE CONTROLLER IS SET TO WARM DURING CRUISE FLIGHT(

PERFORMED BITE CHECK ON DECK SYSTEM IAW FIM. REMOVED AND REPLACED LEFT PACK TEMP CTRL VALVE IAW AMM 21-51-12. OPS CK GOOD AT THIS TIME.

) Next page: https://openairdocs.org/aircraft/N1997A/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 = 'N1997A' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N1997A/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.