# Service difficulty reports: N775UA

A list on [N775UA](https://openairdocs.org/aircraft/N775UA.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 4 · 189 reports

- [SDR CALA2025073007096](https://openairdocs.org/sdr/CALA2025073007096.md): Chiller · no discrepancy · Jul 29, 2025 · N775UA · Boeing 777222 · Buffet/Galleys
  > GALLEY CHILLER IS LOUD AND/OR VIBRATING A3 GALLEY CARRIER 406 OP'S CK'D CHILLER REF MM 25-33-97-700-801, OP'S CK NORMAL, DOES OPERATE LOUDER THAN THE FWD CHILLER BUT NO VISIBLE DEFECTS OR SMELLS
- [SDR CALA2025071806737](https://openairdocs.org/sdr/CALA2025071806737.md): Access Panel · missing · Jul 16, 2025 · N775UA · Boeing 777222 · Nacelle/Pylon, Plate/Skin
  > NUMBER 2 ENGINE INBD PYLON MISSING ACCESS PANEL 443 CL. INSPECTED INSIDE PYLON, NO DAMAGE NOTED. ALL DUCTS SECURE. ONE STRUT PRESSURE RELIEF DOOR MISSING.
- [SDR CALA2025032800500](https://openairdocs.org/sdr/CALA2025032800500.md): Battery · no test · Mar 25, 2025 · N775UA · Boeing 777222 · Emergency Lighting
  > L1 DOOR EMERGENCY LIGHT BATTERY M33424 DEEP CYCLE CHECK FAILED. BATTERY M33424 REPLACED AND TEST NORMAL IAW AMM 33-51 -06.
- [SDR CALA2025032800499](https://openairdocs.org/sdr/CALA2025032800499.md): Charger · no test · Mar 25, 2025 · N775UA · Boeing 777222 · Emergency Lighting
  > R3 DOOR EMERGENCY LIGHT BATTERY CHARGER M33404 TEST FAILED. BATTERY CHARGER M33404 REPLACED AND TESTED NORMAL IAW AMM 33-51-06.
- [SDR CALA2025012301975](https://openairdocs.org/sdr/CALA2025012301975.md): Battery Pack · no test · Jan 22, 2025 · N775UA · Boeing 777222 · Emergency Lighting
  > EMERGENCY LIGHTS - OPERATIONAL TEST WITH THE TEST SWITCHES PROCEDURE - R2 DOOR FWD EMERGENCY EXIT IDENTIFIER SIGN AND ASSOCIATED AISLE PATH EMERGENCY LIGHTS INOP PERFORMED EMERGENCY BATTERY PACK CHARGING PROCEDURE FOR 90 MINUTES REF AMM SUBTASK 33-51-00-860-00
- [SDR CALA2025012402012](https://openairdocs.org/sdr/CALA2025012402012.md): Lamp · inoperative · Jan 20, 2025 · N775UA · Boeing 777222 · Emergency Lighting
  > EMERGENCY LIGHTS - OPERATIONAL TEST WITH THE TEST SWITCHES PROCEDURE - R3, R4 (EXTERIOR) SLIDE LIGHT INOP RELAMPED PER AMM 33-51-04-960-801 CK OK PARTS USED: 767,QTY:1
- [SDR CALA2024061700009](https://openairdocs.org/sdr/CALA2024061700009.md): Tire · worn · Jun 17, 2024 · N775UA · Boeing 777222 · Tire
  > 07 MLG TIRE IS NEARING IT SERVICE LIFE LIMIT TECH MUST MEASURE T HE LOWEST TREAD UPON INITIALIZING PLA AND ENTER THAT MEASURMENT IN THIS LOG. TERMINATING ACTION REQUIRES TIRE REPLACEMENT. INSPECTED TIRE, TREAD WEAR IS AT 1/32 PER AMM, ANY PART OF ANY GROOVE I
- [SDR CALA2024061401798](https://openairdocs.org/sdr/CALA2024061401798.md): Tire · none · Jun 8, 2024 · N775UA · Boeing 777222 · Tire
  > 07 MLG TIRE IS NEARING IT SERVICE LIFE LIMIT TECH MUST MEASURE T HE LOWEST TREAD UPON INITIALIZING PLA AND ENTER THAT MEASURMENT IN THIS LOG. TERMINATING ACTION REQUIRES TIRE REPLACEMENT. VIA SVC 03220 FOR 20 CYCLES. REFERENCE THE APPLICABLE AMM FOR THE TIRE
- [SDR CALA2024050601324](https://openairdocs.org/sdr/CALA2024050601324.md): Battery Pack · no test · May 4, 2024 · N775UA · Boeing 777222 · Emergency Lighting
  > B777-33-3-7015 - M33099 EMERGENCY LT BAT PACK BATTERY CAPACITY FAILED - TRANSFER REFER NON-ROUTINE WO.3168930 AND INSPECTED BY. EMER LT BATTERY REPLACED AND TESTED NORMAL I.A.W AMM 33-51-06 - WORK ACCOMPLISHED BY MECH AND INSPECTED BY IDT INSPECTED OKAY.
- [SDR CALA2024050601315](https://openairdocs.org/sdr/CALA2024050601315.md): Battery · no test · May 4, 2024 · N775UA · Boeing 777222 · Emergency Lighting
  > EMERENCY LT BAT PACK CAPACITY FAILED TANSFER REFER NON-ROUTINE WO.3168932. EMER LIGHT BATTERY PACK REPLACED AND TESTED NORMAL I.A.W AMM33-51-06.
- [SDR CALA2024050601314](https://openairdocs.org/sdr/CALA2024050601314.md): Battery Pack · no test · May 4, 2024 · N775UA · Boeing 777222 · Emergency Lighting
  > B777-33-3-7015 -M33404 EMERENCY BAT PACK BATTERY CAPACITY FAILED TRANSFER REFR NON-ROUTINE WO.3168928 AND ORIGINATED BY M33404 EMER LIGHT BATTERY REPLACED AND TESTED NORMAL I.A.W AMM 33-51-06.
- [SDR CALA2023120103534](https://openairdocs.org/sdr/CALA2023120103534.md): Overheat Loop · loose · Nov 30, 2023 · N775UA · Boeing 777222 · Overheat Detection
  > OVERHEAT CIRCUIT L1 EICAS STATUS LEFT ENGINE OVERHEAT DETECTION CIRCUIT 1 FAILURE. FIM TASK REF: FIM TASK REFERENCE NOT FOUND CMC MSG# 2610131 FLIGHT STATUS: A INTERMITTENCE CODE: H PH: CRUISE NARRATIVE: ENGINE FIRE DETECTION C ARD (LEFT) CMC MSG# 2610141 FLI
- [SDR CALA2023031700769](https://openairdocs.org/sdr/CALA2023031700769.md): Engine · abnormal · Mar 14, 2023 · N775UA · Boeing 777222 · Auto Throttle System
  > ASYMMETRIC THRUST ON T/O RIGHT ENGINE MAX LEFT ENG LAGGED. ACCOMPLISHED "LEFT & RIGHT TMC - AUTOTHROTTLE SERVO LOOP - SYS TEST" PER AMM TASK 22-31-00-730-802-- PASS. ALSO ACCOMPLISHED "TO/GA SW TEST" PER AMM 22-11-00/501 -- OK. PRESENT LEG & FAULT HISTORY ON M
- [SDR CALA2022082602177](https://openairdocs.org/sdr/CALA2022082602177.md): None · none · Aug 26, 2022 · N775UA · Boeing 777 · Lighting System
  > B777-33-3-7019 - DR L2 EMER PWR SUPPLY M33096 CHARGER TEST FAIL TRANSFER REFER NON-ROUTINE WO.933084 - AND ORIGINATED BY V898181 DR L2 M33096 EMER LT BATTERY CHARGER REPLACED AND TESTED NORMAL AS PER AMM 33-51-06 - WORK ACCOMPLISHED BY MECH V898181 AND INSPECT
- [SDR CALA2022082602176](https://openairdocs.org/sdr/CALA2022082602176.md): None · none · Aug 26, 2022 · N775UA · Boeing 777 · Lighting System
  > B777-33-3-7019 DR L2 EMER PWR SUPPLY M33096 BATTERY CAPACITY CHECK FAIL - TRANSFER REFER NON-ROUTINE WO.933076 AND ORIGINATED BY EMP V898181 DR L2 M33096 EMER LIGHT BATTERY REPLACED AND TESTED NORMAL AS PER AMM 33-51-06 - WORK ACCOMPLISHED BY MECH V898181 AND
- [SDR CALA2022082602175](https://openairdocs.org/sdr/CALA2022082602175.md): None · none · Aug 26, 2022 · N775UA · Boeing 777 · Lighting System
  > B777-33-3-7019 DR R3 EMER PWR SUPPLY M33404 BATTERY CAPACITY CHECK FAIL - TRANSFER REFER NON-ROUTINE WO.933072 AND ORIGINATED BY V898181 DR R3 M33404 EMER LIGHT BATTERY REPLACED AND TESTED NORMAL AS PER AMM 33-51-06 WORK ACCOMPLISHED BY MECH V898181 AND INSPEC
- [SDR CALA2018121402567](https://openairdocs.org/sdr/CALA2018121402567.md): Transceiver · malfunctioned · Dec 11, 2018 · N775UA · Boeing 777222 · HF Communications System
  > L AND R HF FAILURE T/S LEFT AND RIGHT HF SYS. FOUND BOTH TUNING PANELS TURN TO DASHES AFTER ATTEMPTING TO TUNE RADIO. REPLACED LEFT HF TXRX. OPS CHECK GOOD. REPLACED RIGHT TXRX. NO DASHES ON TUNING PANEL BUT STILL WOULD NOT CHANNELIZE. OPENED NEW LOG PAGE FOR
- [SDR CALA2018112302414](https://openairdocs.org/sdr/CALA2018112302414.md): Skin · cracked · Nov 23, 2018 · N775UA · Boeing 777222 · Fuselage Main, Plate/Skin
  > REF NR LP 9131011,SUPPORT TASK AD 2017-16-10 EA5310-06900 OP12 RH BS1035 UNDERWING LONGERON FX SKIN AREA 2EA FASTENER HOLES FOUND CRACK AT SKIN,DETAIL REFER ATTACHED FIG ACP PART 1 ECRA 5331-02302 INTERIM REPAIR. WORK ACP ON HAECO HKG NR STS510128 TECH V887387
- [SDR CALA2018112302413](https://openairdocs.org/sdr/CALA2018112302413.md): Structure · cracked · Nov 22, 2018 · N775UA · Boeing 777222 · Fuselage Main, Structure
  > REF NR LP 9131009,SUPPORT TASK AD2017-16-10 EA5310-06900 OP12 RH BS1035 UNDERWING LONGERON RING CHORD AREA,1EA CRACK FOUND AT RA DIUS AT RING CHORD DETAIL REFER ATTACH FIG ACCOMPLISHED PART 1 INTERIM REPAIR PER ECRA 5710-02699 WORK ACOM PLISHED HAECO HKG NR ST
- [SDR CALA2018112302412](https://openairdocs.org/sdr/CALA2018112302412.md): Structure · cracked · Nov 22, 2018 · N775UA · Boeing 777222 · Fuselage Main, Structure
  > REF NR LP 9131010,SUPPORT TASK AD2017-16-10 EA5310-06900 OP12 RH BS1035 UNDERWING LONGERON F/S LOWER CHORD AREA 2EA FASTENER HOLES FOUND CRACK F/S LOWER CHORD,DETAIL REFER ATTACH FIG EA5310-06900 OP12 RH BS1035 UNDERWING LONGERON FRONT SPAR LOWER CHORD REPAIRE
- [SDR CALA2018112302411](https://openairdocs.org/sdr/CALA2018112302411.md): Stringer · cracked · Nov 22, 2018 · N775UA · Boeing 777222 · Fuselage Main, Longeron/Stringer
  > REF NR LP 9130370,SUPPORT TASK - EA5310-06900 OP002 AD2017-16-10 RH BS1035 UNDERWING LONGERON AREA,2EA CRACKS FOUND AT TWO ALUMINUM LAYED AS MARKED RH BS1035 UNDERWING LONGERON REPLACED AS PER EA5310-06900 OP12 SEQ 1470 ADD EMP:V897381 INSP BY HX129800,APPROVE
- [SDR CALA2018102702192](https://openairdocs.org/sdr/CALA2018102702192.md): Battery · discharged · Oct 25, 2018 · N775UA · Boeing 777222 · Emergency Lighting
  > CABIN R3 DOOR EMER LT PWR PACK BATTERY CANNOT BE CHARGED. CABIN R3 DOOR EMER LT PWR PACK BATTERY (M33401) REPLACED AND INSTALLATION TEST CARRIED OUT WITH NORMAL RESULT AS PER AMM 33-51-06.
- [SDR CALA2018102702191](https://openairdocs.org/sdr/CALA2018102702191.md): Battery Pack · discharged · Oct 25, 2018 · N775UA · Boeing 777222 · Emergency Lighting
  > DOOR R3 EMER BATTERY PACK (M33404) CAPACITY CHECK FOUND FAIL. DOOR R3 EMER BATTERY PACK (M33404) BATTERY PACK REPLACED AND INSTALLATION TEST CARRIED OUT WITH NORMAL RESULT AS PER AMM 33-51-06.
- [SDR CALA2018102702190](https://openairdocs.org/sdr/CALA2018102702190.md): Charger · inoperative · Oct 25, 2018 · N775UA · Boeing 777222 · Emergency Lighting
  > DOOR 3R EMER POWER SUPPLY M33404 BATTERY PACK FAILED TO CHARGE UP. DOOR 3R EMER PWR SUPPLY M33404 CHARGER REPLACED AND INSTALLATION TEST CARRIED OUT WITH NORMAL AS PER AMM 33-51-06.
- [SDR CALA2018102202164](https://openairdocs.org/sdr/CALA2018102202164.md): Skin · cracked · Oct 21, 2018 · N775UA · Boeing 777222 · Fuselage Main, Plate/Skin
  > REF NR LP 9130074 SUPPORT TASK AD 2008-16-12 / EA 5300-01986 REV A OP 004 RT STATION 2195.75 BTN STR 5 & STR 10 FOUND CRACKED. PLS ACCOMPLISH OP 010 OF THIS EA. ACCOMPLISHED EA 5300-01986 REV A OP 010 WITH FORM 44-0008, ITEM 1 TO ITEM 14 RII INSPECTED OK APPRO
- [SDR CALA2018102202167](https://openairdocs.org/sdr/CALA2018102202167.md): Skin · cracked · Oct 21, 2018 · N775UA · Boeing 777222 · Fuselage Main, Plate/Skin
  > REF NR LP 9130083 SUPPORT TASK AD 2008-16-12 EA 5300-01986 REV A OP 2 LT STA 2221.65 FX SKIN STR 10 FOUND CRACKED. PLS ACCOMPLISHED OP 8 OF THIS EA ACCOMPLISHED EA 5300-01986 REV A OP 008 WITH FROM 44-0008 ITEM 1 TO ITEM 14 RII INSPECTED OK APPROVED.
- [SDR CALA2018102202166](https://openairdocs.org/sdr/CALA2018102202166.md): Skin · cracked · Oct 21, 2018 · N775UA · Boeing 777222 · Fuselage Main, Plate/Skin
  > REF NR LP 9130084 SUPPORT TASK AD 2008-16-12 / EA 5300-01986 REV A OP1 LT STA 2195.75 BTN STR 5 & 10 FOUND CRACKED. PLS ACCOMPLISHED OP 007 OF THIS EA. ACCOMPLISHED EA 5300-01986 REV A OP 007 WITH FORM 44-0008 ITEM 1 TO ITEM 14 RII INSPECTED OK APPROVED.
- [SDR CALA2018102202165](https://openairdocs.org/sdr/CALA2018102202165.md): Skin · cracked · Oct 21, 2018 · N775UA · Boeing 777222 · Fuselage Main, Plate/Skin
  > REF NR LP 9130075 SUPPORT TASK AD 2008-16-12 / EA 5300-01986 REF A OP 005 RT STATION 2221.65 BTN STR 5 & STR 10 FOUND CRACKED, PLS ACCOMPLISH OP 011 OF THIS EA. ACCOMPLISHED EA 5300-01986 REV A OP 011 WITH FORM 44-0008 ITEM 1 TO ITEM 14 RII INSPECTED OK APPROV
- [SDR CALA2018012200287](https://openairdocs.org/sdr/CALA2018012200287.md): Light · malfunctioned · Jan 22, 2018 · N775UA · Boeing 777222 · Emergency Lighting
  > EMERGENCY LIGHTS ON, IN BACK 1/3 OF CABIN WITH THE SWITCH IN THE ARMED POSITION. COMPLETED SYSTEM RESET, EMERGENCY LIGHTING IN AFT CABIN OFF. IAW SSM 33- 51-15.
- [SDR CALA2017072402356](https://openairdocs.org/sdr/CALA2017072402356.md): Switch · malfunctioned · Jul 24, 2017 · N775UA · Boeing 777222 · Emergency Lighting
  > EMERGENCY LIGHTS AT BOTTOM OF SEATS FROM ROW 48 AFT STAY ON. RESET EMERGENCY LIGHTS SWITCH AT DOOR 4 RT.
- [SDR CALA2017070302092](https://openairdocs.org/sdr/CALA2017070302092.md): Lamp · inoperative · Jul 3, 2017 · N775UA · Boeing 777222 · Emergency Lighting
  > AFT CTR PARTITION ONE EMERGENCY LIGHT INOPERATIVE. REPLACED THE LAMPS, OP CHECKED GOOD.
- [SDR CALA2017060501695](https://openairdocs.org/sdr/CALA2017060501695.md): Connector · loose · Jun 5, 2017 · N775UA · Boeing 777222 · Light System Wiring
  > SEAT EMERGENCY LIGHT AT 33DEFG TO 35DEFG, ON LEFT AND RIGHT SIDE OF SEATS, INOPERATIVE. IAW WDM 33-51-58, FOUND CONNECTOR AT SEAT 36F LOOSE, SECURED THE CONNECTOR, LIGHTS WORKING NORMAL ACCOMPLISHED IDT INSPECTION OF EMERGENCY LIGHT. OPS CHECKED GOOD.
- [SDR CALA2017021700407](https://openairdocs.org/sdr/CALA2017021700407.md): Pressure Deck · cracked · Feb 16, 2017 · N775UA · Boeing 777222 · Fuselage Floor Panel
  > ONE CRACK FOUND AT HORIZONTAL PRESSURE DECK WEB BS 1287 BETWEEN RBL 18.3 AND 25.7, 2.25 INCHES IN LENGTH. REPAIRED IAW EA 5300-01502.
- [SDR CALA2017021700371](https://openairdocs.org/sdr/CALA2017021700371.md): Battery · malfunctioned · Feb 16, 2017 · N775UA · Boeing 777222 · Emergency Lighting
  > L3 DOOR: EXIT SIGN FOUND DIM. THE BATTERY PACK & CHARGER WERE REPLACED. OPS TESTED NORMAL IAW AMM 33-51-06.
- [SDR CALA2017021700394](https://openairdocs.org/sdr/CALA2017021700394.md): Skin · dented · Feb 14, 2017 · N775UA · Boeing 777222 · Passenger/Crew Doors
  > L4 DOOR HAS A DENT IN THE LOWER AFT CORNER. REPAIRED IAW SRM 52-10-01, FIG 102, REPAIR 8.
- [SDR CALA2017021100322](https://openairdocs.org/sdr/CALA2017021100322.md): Battery · discharged · Feb 10, 2017 · N775UA · Boeing 777222 · Emergency Lighting
  > CABIN, ZONE 3, RT EMER AREA LT FOUND DIM (R4 DOOR M33409). ZONE 3, RT EMER LT (M33409) BATTERY AND CHARGER REPLACED AND CHECK NORMAL IAW AMM 33-51-00.
- [SDR CALA2015100194563](https://openairdocs.org/sdr/CALA2015100194563.md): Pressure Switch · malfunctioned · Sep 28, 2015 · N775UA · Boeing 777222 · Landing Gear Brake System
  > PRECAUTIONARY EMER FOR BRAKE ACCUMULATOR PRESS LIGHT. NO FAULTS FOUND IAW FIM. REPLACED BRAKE SOURCE PRESS SWITCH. PERFORMED LEAK CHECK & NO LEAKS. OPERATIONS CHECKED & ALL INDICATIONS NORMAL. NO MSGS DISPLAYED.
- [SDR CALA2014092292258](https://openairdocs.org/sdr/CALA2014092292258.md): Skin · damaged · Sep 22, 2014 · N775UA · Boeing 777222 · Nacelle/Pylon, Plate/Skin
  > NUMBER 1 PYLON OTBD SIDE SKIN HAS WEAR DAMAGE CAUSED BY LATCHES FROM ACCESS PANEL 433CL. ACCOMPLISHED INTERIM REPAIR IAW ECRA 5451-01167 PART 1. INITIAL HFEC INSPECTION REQUIRED WITHIN 16419 CYCLES FROM PTC 13581 & REPEAT AT EVERY 12000 CYCLES THEREAFTER IAW
- [SDR CALA2014070191386](https://openairdocs.org/sdr/CALA2014070191386.md): Unknown · malfunctioned · Jul 1, 2014 · N775UA · Boeing 777222 · Windshield/Door Rain/Ice Removal
  > WINDOW HEAT RT SIDE INOPERATIVE. CYCLED IAW CHECKLIST, STILL INOPERATIVE. FOUND INACTIVE MX MSG 30-22031. IAW FIM MAN 30-41-813, RT SIDE NR 2 WINDOW HEAT NORMAL BUT HAD AN INTERMITTENT FAULT. UNLATCHED EICAS MSG, INOPERATIVE LIGHTS ON OVERHEAD PANEL WINDOW
- [SDR CALA2014012790231](https://openairdocs.org/sdr/CALA2014012790231.md): Transducer · faulty · Jan 27, 2014 · N775UA · Boeing 777222 · Brake Anti-Skid Section
  > ANTI-SKID TRANSDUCER LT STATUS MESSAGE ACTIVE MTC MESSAGE 32-30300. FAULTING WHEEL SPEED TRANSDUCER NR 6. HAS HISTORY INCLUDING TRANSDUCER REPLACEMENT. SEE PTT SEQ 6162007 NR 6 TRANSDUCER REPLACED. POSSIBLY BAD FROM STOCK OR WIRING.
- [SDR CALA2013112193153](https://openairdocs.org/sdr/CALA2013112193153.md): Wire · unsecure · Nov 18, 2013 · N775UA · Boeing 777222 · Flight Control System Wiring
  > ONE OR MORE PFCS INTERFACE SIGNALS INOPERATIVE. SECURED JUMPER WIRE BETWEEN CB C23403 & C9117 IN P210. ALL MESSAGES CLEARED SYS OPERATIONS NORMAL.
- [SDR CALA2013111292870](https://openairdocs.org/sdr/CALA2013111292870.md): Sdu · faulty · Nov 8, 2013 · N775UA · Boeing 777222 · Communications System
  > SATCOM SDU ISSUE, RTFL. REPLACED SATCOM SDU IAW MM. MR23816-26 OFF, 61 ON. STILL REQUIRES INSTALLATION TEST.
- [SDR CALA2013102992471](https://openairdocs.org/sdr/CALA2013102992471.md): Skin Panel · unsecure · Oct 26, 2013 · N775UA · Boeing 777222 · Wing, Plate/Skin
  > RT WING, WING ANTI ICE PANEL HANGING DOWN, OTBD OF PANEL 621AB. REPLACED RT WING OTBD FIXED LE LOWER SKIN PANEL THERM ANTI-ICE, OPERATIONS CHECKED OF SLATS OK.
- [SDR CALA2013100891857](https://openairdocs.org/sdr/CALA2013100891857.md): Oven · dirty · Oct 8, 2013 · N775UA · Boeing 777222 · Buffet/Galleys
  > SMOKE COMING FROM OVEN WARMER W51 AFT GALLEY. ONLY FOUND SPILLED & MELTED CHOCOLATE SYRUP, NO ELECTRICAL HAZARD. SOURCE OF SMOKE IAW IADMM WAS THE SPILLED SYRUP. IAD VERIFIED NO OTHER DEFECTS WITH THE OVEN. OVEN INOPERATIVE TILL SYRUP CAN BE PROPERLY CLEAN
- [SDR CALA2013092691487](https://openairdocs.org/sdr/CALA2013092691487.md): Pump · inoperative · Sep 22, 2013 · N775UA · Boeing 777222 · APU Engine Fuel and Control
  > EICAS STATUS MESSAGE APU DISPLAYED. ACCOMPLISHED TROUBLESHOOTING IAW MAINTENANCE MESSAGE 49-07950, FOUND APU DC PUMP INOPERATIVE. ITEM DEFERRED IAW MEL 2825B PULLED CB P310B1 & INSTALLED COLLAR. REPLACED APU DC FUEL PUMP, CHECKED GOOD.
- [SDR CALA2013082090575](https://openairdocs.org/sdr/CALA2013082090575.md): Ace · malfunctioned · Aug 19, 2013 · N775UA · Boeing 777222 · Drag Control System
  > SPOILER FAILURE OF ONE OR MORE SPOILER PAIRS. REMOVED AND REPLACED RIGHT ACE, IAW AMM. OPS CHECKED OK. NO STATUS MESSAGE NOTED.
- [SDR UALA2013062704518](https://openairdocs.org/sdr/UALA2013062704518.md): Switch · faulty · Jun 26, 2013 · N775UA · Boeing 777222 · Windshield/Door Rain/Ice Removal
  > WINDOW HEAT LT SIDE LOSS OF LT SIDE WINDOW HEAT ADVISORY. REPLACED LT WINDOW HEAT SWITCH, CKS OK-PASSED WINDOW HEAT SYS TEST ON MAT.
- [SDR UALA2013061704154](https://openairdocs.org/sdr/UALA2013061704154.md): Skin · dented · Jun 14, 2013 · N775UA · Boeing 777222 · Fuselage Main, Plate/Skin
  > CUSTOMER SERV AGENT REPORTS DENT, 4 FT FWD OF 2L ENTRY DOOR JUST BELOW FLOOR LINE. SMALL DENT 5" BELOW FLOOR LINE AT STA 680, DIM 1.875 IN WIDE BY.050". SMOOTH WITH NO CRACK OR OTHER DAMAGE. WITHIN LIMITS IAW SRM 53-00-01, FIG 10 2, DETAIL E, PG 108.
- [SDR UALA2013052903740](https://openairdocs.org/sdr/UALA2013052903740.md): Line · leaking · May 28, 2013 · N775UA · Boeing 777222 · Hydraulic System, Main
  > FOUND HYDRAULIC LEAK COMING FROM RT MLG (UPPER AREA). FOUND LEAK COMING FROM FLEX LINE ON RT MLG ANTI-SKID BRAKE LINE. REPLACED FLEX LINE. SERVICED HYD SYS TO FULL. LEAK CHECKED, FOUND NO LEAKS.
- [SDR UALA2013041502535](https://openairdocs.org/sdr/UALA2013041502535.md): Starter · faulty · Apr 12, 2013 · N775UA · Boeing 777222 · APU Start/Ignition System
  > ON APU START UP, WITH BATTERY VOLTAGE AT 31 VOLTS, APU NO LIGHT OFF. NO ROTATION. APUC MESSAGE RPM BELOW 7% AND AUTO SHUT DOWN. NO BATTERY VOLTAGE DROP WHILE CRANKING. REPLACED APU STARTER PER MM. ALSO REPLACED APUC PER MM. APU STARTED ON FIRST ATTEMPT W

Next page: https://openairdocs.org/aircraft/N775UA/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 = 'N775UA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N775UA/reports

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