# Service difficulty reports: Boeing 777-2Q8

A list on [Boeing 777-2Q8](https://openairdocs.org/model/boeing-777-2q8.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 2 · 67 reports

- [SDR ASMF201801007](https://openairdocs.org/sdr/ASMF201801007.md): Seal · leaking · Dec 2, 2017 · N774AM · Boeing 7772Q8 · Nose/Tail Landing Gear Strut/Axle
  > DURING A TRANSIT CHECK, FOUND A HYDRAULIC LEAK IN THE NOSE LANDING GEAR. THE NOSE LANDING GEAR SHOCK STRUT HYDRAULIC LEAK OUT OF LIMITS. THE SEALS WERE REPLACED IAW AMM 32-21-25, TESTED CORRECT.
- [SDR ASMF20170911009](https://openairdocs.org/sdr/ASMF20170911009.md): Pcu · leaking · Aug 28, 2017 · N774AM · Boeing 7772Q8 · Drag Control Actuator
  > DURING TRANSIT CHECK, DETECTED EVIDENCE OF A HYDRAULIC LEAK IN THE LEFT MAIN LANDING GEAR. MAINTENANCE PERSONNEL PERFORMED INSPECTION IAW AMM 27-61-00, DETECTING A LEAK IN THE INBOARD SPOILER POWER CONTROL ACTUATOR, THE POWER CONTROL UNIT NR 7 WAS REPLACED IAW
- [SDR ASMF20170531005](https://openairdocs.org/sdr/ASMF20170531005.md): Monitor · damaged · May 27, 2017 · N745AM · Boeing 7772Q8 · Flight Control System
  > AIRCRAFT RETURNED TO PLATFORM DUE TO DURING TAKE OFF, CONFIGURATION STABILIZER ALARM WAS ACTIVED. MAINTENANCE PERSONNEL PERFORMED INSPECTION IAW FIM 31-43 TASK 867, CONFIRMING FAILURE IN IOM 003 RH OF INVALID DATA, THEREFORE THE IOM M003 RIGHT WAS REPLACED IAW
- [SDR ASMF201705002](https://openairdocs.org/sdr/ASMF201705002.md): Pump · failed · May 16, 2017 · N745AM · Boeing 7772Q8 · Aircraft Fuel Distribution System
  > CAPTAIN REPORTED THAT DURING CRUISE, THE FUEL QUANTITY INDICATION WAS WRONG, FUEL QUANTITY WAS VERIFIED USING FUEL DIPSTICK. OPS TESTED FOR THE SYSTEM FUEL QUANTITY INDICATOR PERFORMED IAW AMM 28-24-00, FUEL TRANSFER WHEN NOT COMMANDED WAS PERFORMED IAW FIM 2
- [SDR ASMF201611015](https://openairdocs.org/sdr/ASMF201611015.md): Carbon Seal · leaking · Sep 25, 2016 · N776AM · Boeing 7772Q8 · Engine Oil Cooler
  > CAPTAIN REPORTED THAT DURING APPROACH, THE LEFT ENGINE OIL QUANTITY DECREASED TO 3 QTS WITH ENGINE PARAMETERS NORMAL. THE AIRCRAFT WAS SENT TO THE HANGAR AND MAINTENANCE PERSONNEL PERFORMED LEFT ENGINE LEAK CHECK IAW AMM 71-00-00-700-823, AMM 79-00-00-200-800,
- [SDR ASMF201608008](https://openairdocs.org/sdr/ASMF201608008.md): Window · cracked · Jul 5, 2016 · N746AM · Boeing 7772Q8 · Flight Compartment Windows
  > CAPTAIN REPORTED THAT DURING CRUISE, THE RT SIDE WINDOW HEAT WITH FAULT CODE 304 022 42 DUE TO A CRACK ON THE LOWER RT CORNER WITH CORRECT CABIN PRESSURE. MAINTENANCE REPLACED THE RIDE SIDE OPERABLE WINDOW IAW AMM 56-11-02, TESTED CORRECT.
- [SDR ASMF201608002](https://openairdocs.org/sdr/ASMF201608002.md): Coupler · leaking · Jun 19, 2016 · N774AM · Boeing 7772Q8 · Waste Disposal System
  > DURING TRANSIT CHECK, A WATER LEAK WAS DETECTED IN THE LOWER FUSELAGE. MAINTENANCE PERSONNEL PERFORMED REVISION DETECTING WATER LEAK IN THE LT AFT CARGO COMPARTMENT LINE AND COVER AND IN AFT DRAIN VALVE LINE. THE COVER, COUPLER AND DRAIN VALVE LINE SEALS WER
- [SDR ASMF20160620011](https://openairdocs.org/sdr/ASMF20160620011.md): Transceiver · failed · May 6, 2016 · N776AM · Boeing 7772Q8 · Weather Radar System
  > AIRCRAFT PERFORMED AN UNSCHEDULED LANDING DUE TO EICAS MESSAGE WXR FAIL. MAINTENANCE PERFORMED THE AIR/GROUND INTERFACE TEST IAW AMM 34-43-02, DETECTING WXR FAIL FLAG AND WXR SYS STATUS; SO THE LT TRANSCEIVER WAS REPLACED AND SYSTEM TEST WAS PERFORMED IAW AMM
- [SDR ASMF201606003](https://openairdocs.org/sdr/ASMF201606003.md): Brake Assy · overheated · Apr 17, 2016 · N774AM · Boeing 7772Q8 · Brake
  > AIRCRAFT REJECTED TAKEOFF AT 100 KNOTS DUE TO AN EVENT OF 1023 DEGREES CELSIUS OF EGTS EXCEEDANCE IN THE FELT ENGINE AND BY NOTIFICATION OF THE AIR TRAFFIC CONTROL OF FIRE EVIDENCE IN THE RT MLG. THE ACFT WAS SENT TO HANGAR AND MAINTENANCE PERSONNEL PERFORMED
- [SDR ASMF201602009](https://openairdocs.org/sdr/ASMF201602009.md): Windshield · cracked · Feb 3, 2016 · N776AM · Boeing 7772Q8 · Flight Compartment Windows
  > AIRCRAFT RETURNED FROM FLIGHT DUE TO, DURING CLIMB THE RT WINDSHIELD GOT CRACKED. PERFORMED THE QRH 1.9 PROCEDURE, CONFIRMING THE FAILURE. ACFT WAS SENT TO THE HANGAR & MX REPLACED THE LT L1 WINDSHIELD ASSEMBLY IAW MM 56-11-01 & WINDOW HEAT SYS TEST WAS PERF
- [SDR ASMF201602007](https://openairdocs.org/sdr/ASMF201602007.md): Hydraulic Line · leaking · Jan 24, 2016 · N745AM · Boeing 7772Q8 · Hydraulic System, Main
  > CAPTAIN REPORTED THAT DURING APPROACH, THE HYD CENTRAL SYS QTY DECREASED TO 0.14 GAL & THE MSG IN EICAS & STATUS OF AUTO BRAKE SOL VLV WAS SHOWN. PERFORMED ACFT TURN AROUND, DETECTING HYD LEAK IN LT MLG HOSE. THE HOSE WAS REPLACED IAW AMM 20-10-14 & AMM 32-3
- [SDR ASMF201602001](https://openairdocs.org/sdr/ASMF201602001.md): Slide Raft · stuck · Dec 20, 2015 · N774AM · Boeing 7772Q8 · Escape Slide
  > DURING TRANSIT CHECK, THE LT DOOR SLIDE, RAFT NR 1 WAS FOUND STUCK & OUT OF POSITION. REMOVED THE LT DOOR SLIDE, RAFT NR 1 IAW AMM 25-66-01 & DEFERRED THE LT DOOR NR 1 IAW MEL 52-11-01-01A, CAT A, WITH THE CORRESPONDING RESTRICTION OF BLOCK 80 SEATS. THE LT
- [SDR ASMF201511009](https://openairdocs.org/sdr/ASMF201511009.md): Actuator Valve · failed · Nov 12, 2015 · N774AM · Boeing 7772Q8 · Aircraft Fuel Distribution System
  > AIRCRAFT RETURNED TO PLATFORM DUE TO DURING LT ENG START THE MSG IN EICAS & STATUS OF ENG FUEL VLV LT, SPAR VLV LT & LIGHTS TURNED ON. PERFORMED FIM 28-20 TASK 801 PROCEDURE, DETECTING THE LT SPAR VLV ACTUATOR FAILED. THE LT SPAR VLV ACTUATOR WAS REPLACED IA
- [SDR ASMF201511008](https://openairdocs.org/sdr/ASMF201511008.md): Actuator Valve · failed · Nov 11, 2015 · N776AM · Boeing 7772Q8 · Engine Fuel Distribution
  > AIRCRAFT RETURNED TO PLATFORM DUE TO DURING TAXING, THE RT ENG FAIL LIGHT TURNED ON WITHOUT ABNORMAL INDICATIONS & DURING THE RT ENG SHUTDOWN, THE EGT EXCEEDANCE WAS SHOWN. PERFORMED FIM 73-11 TASK 815 & FIM 73-22 TASK 815 & 820 PROCEDURES & IDLE POWER OPERAT
- [SDR ASMF201510028](https://openairdocs.org/sdr/ASMF201510028.md): Tire · punctured · Oct 9, 2015 · N776AM · Boeing 7772Q8 · Tire
  > AIRCRAFT RETURNED TO PLATFORM DUE TO MSG IN EICAS & STATUS OF LOW PRESS IN TIRE NR 11. PERFORMED REVISION DETECTING THE TIRE NR 11 WITH PRESS DROPPED OFF TO 26 PSI DUE TO DRILLING. WHEEL NR 11 WAS REPLACED IAW AMM 32-45-00, ALL CORRECT.
- [SDR ASMF201507018](https://openairdocs.org/sdr/ASMF201507018.md): Wire · damaged · Jun 29, 2015 · N776AM · Boeing 7772Q8 · Engine Fuel System Wiring
  > AIRCRAFT RETURNED TO PLATFORM, DURING LT ENG START, THE FAILURE CODE 73 21 52 51 & 732 152 51 WERE SHOWED & LT ENG NOT STARTED BY TWO ATTEMPTS. PERFORMED REVISION TO LT ENG, DETECTING LT HIGH PRESS FUEL SOV POSITION IN DISAGREE WITH COMMAND POSITION. THE FIM
- [SDR ASMF201506012](https://openairdocs.org/sdr/ASMF201506012.md): Radome · out of limits · May 15, 2015 · N774AM · Boeing 7772Q8 · Aerodynamic Fairings
  > AIRCRAFT PERFORMED AN UNSCHEDULED LANDING DUE TO DURING CLIMB EICAS MSG WXR FAIL & BOTH WX RADARS DID NOT SHOW INDICATIONS CORRECT. PERFORMED A BIRD & HAIL STRIKE CONDITIONAL INSPECTION IAW MM 05-51-18, DETECTING FOD IN THE RADOME & IT WAS FOUND OUT OF LIMITS
- [SDR ASMF201503012](https://openairdocs.org/sdr/ASMF201503012.md): Valve · loose · Feb 6, 2015 · N745AM · Boeing 7772Q8 · Landing Gear Brake System
  > DURING TRANSIT CHECK, IT WAS DETECTED A HYD LEAK IN THE WHEEL NR 4. DURING MX REVISION, THE WHEEL NR 4 WAS DETECTED LEAKING WITHIN LIMITS. THE BRAKES BLEED PORT OF THE WHEEL NR 4 WAS TIGHTENED & CLEANED IAW AMM 32-45-00, TESTED CORRECT.
- [SDR ASMF201501011](https://openairdocs.org/sdr/ASMF201501011.md): Generator · failed · Nov 4, 2014 · N746AM · Boeing 7772Q8 · AC Generator-Alternator
  > CAPTAIN REPORTED THAT AFTER START ENGS APPEARED THE EICAS MSG LT BACK UP GEN OUT OF SERVICE. PERFORMED FIM 24-20 TASK 811 PROCEDURE, SHOWING FAILURE CODE 24-46000. THE BACK GEN WAS DEFERRED IAW MEL 24-25-01A CAT C. REPLACED THE BACK GEN IAW AMM 24-25-01, TE
- [SDR ASMF201409009](https://openairdocs.org/sdr/ASMF201409009.md): Idg · leaking · Aug 27, 2014 · N774AM · Boeing 7772Q8 · AC Generator-Alternator
  > CAPTAIN REPORTED THAT AFTER START ENGS, THE EICAS MSG ELEC GEN SYS R WAS SHOWN & THE RT DRIVE LIGHT TURNED ON. DURING MAINTENANCE REVISION, AN OIL LEAK WAS DETECTED IN THE INTEGRATED DRIVE GENERATOR SEALS DRAIN. THE RT INTEGRATED DRIVE GENERATOR WAS DEFERRED
- [SDR ASMF201407008](https://openairdocs.org/sdr/ASMF201407008.md): Bracket · broken · Jul 1, 2014 · N745AM · Boeing 7772Q8 · Main Landing Gear Strut/Axle/Truck
  > AIRCRAFT PERFORMED AN UNSCHEDULED LANDING DUE TO URGENT ATTENTION OF A SICK PAX. PERFORMED AN OVERWEIGHT LANDING INSPECTION IAW MM 05-51-35 PHASE 1, DETECTING A RT MLG HYD TRUCK BRACKET BROKEN. EVALUATED THE DAMAGE & FOUND IT WITHIN LIMITS IAW AMM 32-10-01.
- [SDR ASMF201407003](https://openairdocs.org/sdr/ASMF201407003.md): Skin · dented · Jun 15, 2014 · N774AM · Boeing 7772Q8 · Fuselage Main, Plate/Skin
  > DURING OVERNIGHT CHECK, DETECTED A BIRD STRIKE ABOVE FUSELAGE WINDSHIELD, SO BIRD STRIKE CONDITIONAL INSPECTION WAS PERFORMED IAW MM 05-51-18, DETECTING A DENT OF 10.0 INCHES LONG, 4.5 INCHES WIDE & 0.074 INCHES DEPTH, BETWEEN STATIONS 204.5 & 2 LBL22. EVALUA
- [SDR ASMF201407001](https://openairdocs.org/sdr/ASMF201407001.md): Static Port · damaged · Jun 1, 2014 · N774AM · Boeing 7772Q8 · Pitot/Static System
  > DURING TRANSIT CHECK DETECTED EVIDENCE OF A LIGHTNING STRIKE IN THE RT ENG STATIC PORT. PERFORMED A LIGHTNING STRIKE INSPECTION IAW MM 05-51-19 DETECTING THE STATIC PORT DAMAGED, SO THE STATIC PORT WAS REPLACED IAW CMM 71-11-36, TESTED CORRECT.
- [SDR ASMF2014061706010](https://openairdocs.org/sdr/ASMF2014061706010.md): Slide Raft · out of position · Apr 27, 2014 · N745AM · Boeing 7772Q8 · Escape Slide
  > DURING TRANSIT CHECK, THE LT DOOR SLIDE RAFT NR 2 WAS FOUND OUT OF POSITION ON THE ACFT FLOOR & WITH METAL SEAMS LOOSEN. ACFT WAS SENT TO THE HANGAR & SENT THE LT DOOR SLIDE RAFT TO SURVIVAL SHOP FOR ASSEMBLY CORRECTLY IAW CMM 25-61-52. INSTALLED THE RT DOOR
- [SDR ASMF201311223002](https://openairdocs.org/sdr/ASMF201311223002.md): Warning System · false activation · Dec 18, 2013 · N746AM · Boeing 7772Q8 · Central Computers
  > AIRCRAFT PERFORMED AN UNSCHEDULED LANDING AT LIM DUE TO EICAS MESSAGE WXR SYS. MX PERSONNEL PERFORMED THE AIR, GND INTERFACE TEST IAW AMM 34-43-00, NOT CONFIRMING THE FAILURE & DELETING FAILURE MESSAGE, THE WXR SYS TEST WAS PERFORMED IAW AMM 34-43-00, TESTED
- [SDR ASMF201312005](https://openairdocs.org/sdr/ASMF201312005.md): Engine · malfunctioned · Dec 1, 2013 · N746AM · Boeing 7772Q8 · Engine (Turbine/Turboprop)
  > CAPTAIN REPORTED THAT DURING TAKEOFF, THE RT ENG REACHED 1031 CELSIUS DEGREES OF EGT FOR AROUND 2 SECONDS. PERFORMED RT ENG INSPECTION WITH EGT PARAMETERS WITHIN OPERATION LIMITS IAW AMM 71-00-00 & ENG EXCEEDANCE CHECK IAW AMM 71-00-00, TESTED CORRECT.
- [SDR ASMF201311011](https://openairdocs.org/sdr/ASMF201311011.md): Shutoff Valve · malfunctioned · Nov 5, 2013 · N774AM · Boeing 7772Q8 · Fuel Selector/Shut-Off Valve
  > DURING FUELING FOR PUMP JETTISON TEST, A FUEL SPILLAGE IN THE RT TANK OCCURRED DUE TO THE SHUTOFF VLV DID NOT CLOSE. THE PLATFORM WAS CLEANED BY FIREMEN & MX PERSONNEL CLEANED THE VLV & IT WAS TESTED SEVERAL TIMES IAW MM 28-13-00, NO LEAK WAS DETECTED & SHUTOF
- [SDR ASMF201310005](https://openairdocs.org/sdr/ASMF201310005.md): Radome · deformed · Sep 19, 2013 · N776AM · Boeing 7772Q8 · Aerodynamic Fairings
  > DURING TRANSIT CHECK, FOUND RADOME DEFORMED. FOUND OUT OF LIMITS IAW SRM 57-12-00. RADOME REPLACED IAW AMM 57-12-02.
- [SDR ASMF201308016](https://openairdocs.org/sdr/ASMF201308016.md): Fairing · damaged · Jul 24, 2013 · N746AM · Boeing 7772Q8 · Engine Thrust Reverser
  > CAPTAIN REPORTED THAT DURING LANDING ROLL, ACFT HAD A BIRD STRIKE ON RT ENGINE. MX PERSONNEL PERFORMED A BIRD STRIKE CONDITIONAL INSPECTION IAW MM 05-51-18, DETECTING RT ENGINE REVERSER CASCADE SEGMENT NR 8 DAMAGED AND OGV FAIRING WITH SCRATCHES. INSPECTION
- [SDR ASMF201308008](https://openairdocs.org/sdr/ASMF201308008.md): Fairing · damaged · Jul 12, 2013 · N745AM · Boeing 7772Q8 · Wing Structure
  > DURING TRANSIT CHECK, A BIRD STRIKE WAS DETECTED IN RT ENGINE. BIRD STRIKE CONDITIONAL INSPECTION WAS PERFORMED IAW MM 05-51-18, DETECTING 6 FAIRING DAMAGES AND 2 PANELS WITH 4 IMPACT, BEING WITHIN LIMITS OF OPERATION IAW AMM 71-00-00. PANELS WERE REPAIRED I
- [SDR ASMF201308006](https://openairdocs.org/sdr/ASMF201308006.md): Structure · damaged · Jul 9, 2013 · N746AM · Boeing 7772Q8 · Landing Gear Doors
  > DURING ROUTINE CHECK, LIGHTNING STRIKE IN NOSE AND MLG. MAINTENANCE PERSONNEL PERFORMED A LIGHTNING STRIKE INSPECTION IAW MM 05-51-19, DETECTING VHF ANTENNA NR 2 WITH DAMAGE OUT OF LIMIT, THREE BURNS IN THE FWD LEFT NLG DOOR AND TWENTY BURNS IN THE LT MLG DOO
- [SDR ASMF201306003](https://openairdocs.org/sdr/ASMF201306003.md): Wedge · cracked · Jun 2, 2013 · N776AM · Boeing 7772Q8 · Trailing Edge Flaps
  > DURING TRANSIT CHECK, THE T/E WEDGE RT OTBD FLAP WAS DAMAGED PROMOTING A CRACK OF 6.00" LENGTH AND 5.75" WIDE AT BS 214, ON UPPER & LOWER RT OTBD FLAP. MX PERSONNEL ISSUED THE NON ROUTINE CARD A0205977. THE T/E WEDGE RT OTBD FLAP WAS REPAIRED IAW SRM 57-53-0
- [SDR ASMF20130531012](https://openairdocs.org/sdr/ASMF20130531012.md): Line · leaking · May 15, 2013 · N774AM · Boeing 7772Q8 · Hydraulic System, Main
  > CAPTAIN REPORTED THAT DURING LANDING, A HYD LEAK WAS DETECTED IN THE RT HYD SYS WITH INDICATION OF 30 PERCENT. MX PERSONNEL PERFORMED REVISION DETECTING HYD LEAK AT RT EDP HOUSE ASSY HYD SUPPLY LINE. HYD SUPPLY LINE WAS REPLACED IAW AMM 29-11-06 AND TEST NU
- [SDR ASMF201303017](https://openairdocs.org/sdr/ASMF201303017.md): Actuator · leaking · Feb 8, 2013 · N746AM · Boeing 7772Q8 · Drag Control Actuator
  > DURING TRANSIT CHECK, A HYD LEAK WAS DETECTED ON AFT REAR SPAR OF LT WING. MX PERSONNEL PERFORMED AN INSPECTION DETECTING HYD LEAK IN SPOILER ACTUATOR NR 3, SO THE ACTUATOR WAS REPLACED IAW AMM 27-61-08 AND ADJUSTMENT AND TEST WERE PERFORMED IAW AMM 27-61-00,
- [SDR ASMF201211007](https://openairdocs.org/sdr/ASMF201211007.md): Probe · malfunctioned · Nov 18, 2012 · N745AM · Boeing 7772Q8 · Engine EGT/TIT Indicating System
  > ACFT RETURNED TO PLATFORM DUE TO AFTER RT ENGINE START, IT WAS HAD OSCILLATIONS BETWEEN 540 AND 580 CELSIUS DEGREES OF EGT. ACFT WAS SENT TO THE HANGAR AND MX PERSONNEL REPLACED THE LOWER AND UPPER EGT PROBES AND HARNESS T-49 IAW MM 77-21-01 AND 77-21-05, TES
- [SDR ASMF201211006](https://openairdocs.org/sdr/ASMF201211006.md): Bypass Valve · failed · Nov 16, 2012 · N774AM · Boeing 7772Q8 · Steering Unit
  > ACFT RETURNED TO PLATFORM DUE TO DURING TAXING THE NOSE WHEEL STEERING WAS STUCK. MX PERSONNEL PERFORMED THE FIM 32-51 TASK 808 PROCEDURE, DETECTING THE BY PASS VALVE STUCK; SO THE VALVE ASSY WAS LUBRICATED IAW MM 31-51-07, TESTED CORRECT.
- [SDR ASMF201210009](https://openairdocs.org/sdr/ASMF201210009.md): Engine · intermittent · Sep 29, 2012 · N776AM · Boeing 7772Q8 · Engine (Turbine/Turboprop)
  > ACFT REJECTED TAKE AT 70 KNOTS WITH A GROSS WEIGHT OF 268 000 KG DUE TO RIGHT ENGINE STRONG EXPLOSION WITHOUT ADVISE ON ENGINE PARAMETERS OR EXCEEDS IN CREW CABIN WAS LISTENING. MX PERFORMED FIM 71-05 TASK 807 PROCEDURE; A RT ENGINE STALL INSPECTION IAW MM 71
- [SDR ASMF201207009](https://openairdocs.org/sdr/ASMF201207009.md): Panel · punctured · Jul 31, 2012 · N776AM · Boeing 7772Q8 · Nacelle/Pylon, Main Frame
  > DURING TRANSIT CHECK, DAMAGE WAS DETECTED IN THE NOSE COWLING SKIN ACOUSTIC PANEL OF THE LT ENGINE, A PUNCTURE 1 X 0.75 INCH BEING OUT OF LIMITS IAW SRM 54-11-01. THE DAMAGE WAS REPAIRED IAW AMX-12-0324-02B, TESTED CORRECT.
- [SDR ASMF201207001](https://openairdocs.org/sdr/ASMF201207001.md): Skin · punctured · Jun 19, 2012 · N746AM · Boeing 7772Q8 · Wing, Plate/Skin
  > DURING PUSH BACK, THE LT WING L/E WAS HIT BY A MOBILE STAIRWAY CAUSING A HOLE OF 8.0" LONG, 4.0" WIDE. INSPECTION PERSONNEL EVALUATED THE DAMAGED AND FOUND OUT LIMITS IAW SRM 57-41-00. MX ISSUED THE NON ROUTINE CARDS A0190507 AND A019506. THE MID FAIRING AS
- [SDR ASMF201205001](https://openairdocs.org/sdr/ASMF201205001.md): Connector · damaged · Apr 27, 2012 · N774AM · Boeing 7772Q8 · Communications System Wiring
  > DURING OVERNIGHT CHECK, THE EMERGENCY LOCATOR TRANSMITTER ACTIVATED INTERMITTENTLY WITH ELT SWITCH IN OFF POSITION. MX PERSONNEL REMOVED THE EMERGENCY LOCATOR TRANSMITTER IAW MM 23-24-01. ELT INSTALLED IAW MM 23-24-01 AND CONNECTOR DM23575A WAS REPLACED IAW
- [SDR ASMF201110002](https://openairdocs.org/sdr/ASMF201110002.md): Unknown · smoke · Oct 6, 2011 · N776AM · Boeing 7772Q8 · Air Distribution System
  > DURING CLIMB, SMOKE IN THE PASSENGER CABIN ON THE PREMIER CLASS AND THE FIRST 20 ROWS WAS VISIBLE ALONG THE CEILING; SO FLIGHT CREW ACCOMPLISHED THE QRH 8.5 PROCEDURE. ACFT RETURNED, MX PERSONNEL PERFORMED SMOKE OR FUMES IN CABIN CONDITIONAL INSPECTION IAW MM
- [SDR ASMF201106001](https://openairdocs.org/sdr/ASMF201106001.md): Sensor · damaged · Jun 1, 2011 · N745AM · Boeing 7772Q8 · Cabin Cooling System
  > AIRCRAFT RETURNED DURING CLIMB, THE EICAS MESSAGE LT PACK WAS SHOWN AND IT WAS NOT AIR ON LT DUCT. DURING MX REVISION, THE MESSAGES 21-23041 WAS SHOWN, THE FIM 21-51 TASK 803 PROCEDURE WAS PERFORMED; SO THE LT PACK SENSOR WAS REPLACED IAW MM 21-51-03, TESTED C
- [SDR ASMF201105001](https://openairdocs.org/sdr/ASMF201105001.md): O-Ring · cracked · Apr 28, 2011 · N774AM · Boeing 7772Q8 · Fuel Boost Pump
  > DURING TRANSIT CHECK, TECH PERSONNEL DETECTED A FUEL LEAK IN RT WING DUE TO A CRACK IN THE FUEL PUMP O-RING NR 3; SO THE RT FUEL PUMP O-RING WAS REPLACED IAW MM 28-31-01, TESTED CORRECT.
- [SDR ASMF201104002](https://openairdocs.org/sdr/ASMF201104002.md): Pump · leaking · Apr 4, 2011 · N776AM · Boeing 7772Q8 · Hydraulic Pump (Electric/Engine), Main
  > CAPTAIN REPORTED THAT DURING CRUISE, THE HYD QTY LOW LT AND HYD PRESS PRI LT LIGHTS TURNED ON. THE FLIGHT CREW PERFORMED THE QRH 13.3 AND 13.22 PROCEDURES, CONFIRMING THE FAILURE AND CONTINUING TO DESTINATION. MX PERSONNEL, A REVISION, DETECTING HYD LEAK IN TH
- [SDR ASMF20110322001](https://openairdocs.org/sdr/ASMF20110322001.md): Bolt · loose · Mar 22, 2011 · N774AM · Boeing 7772Q8 · Engine (Turbine/Turboprop)
  > CAPTAIN REPORTED DURING THE DESCENT, THE RT ENGINE VIBRATION REACHED 4.7 OF N2. ACFT WAS SENT TO THE HANGAR AND MX PERFORMED A TRIM BALANCE IAW MM 71-00-00 TASK 71-00-00-700-847-G01 DETECTING 6 RT ENGINE FAN WEIGHT BALANCE BOLTS WERE LOOSE AT THE 5, 11, 12,
- [SDR ASMF201102003](https://openairdocs.org/sdr/ASMF201102003.md): Blades · damaged · Feb 14, 2011 · N774AM · Boeing 7772Q8 · Turbine Engine Compressor Section
  > DURING A BORESCOPE INSPECTION OF THE HPC 1ST STAGE BLADES OF RIGHT ENGINE WAS DETECTED FOUR BLADES OF THE HPC 1ST STAGE WITH LEADING EDGE TIP CURLED 45 DEGREES OUT OF LIMITS IAW 72-00-00, PARAGRAPH 5H (8) C (7), PAGE 625; WITH DIMENSIONS OF 1.0 INCHES LENGTH A
- [SDR ASMF201012009](https://openairdocs.org/sdr/ASMF201012009.md): Tire · damaged · Dec 17, 2010 · N774AM · Boeing 7772Q8 · Tire Tube
  > DURING TOWING TO PLATFORM, THE TOW TRACTOR DRIVER WAS EXCEEDING THE MAXIMUM NLG TOWING ANGLE TO LT SIDE AND TOW BAR WAS BROKEN. MX PERFORMED THE MAXIMUM NLG TOWING ANGLE CONDITIONAL INSP IAW MM 05-51-29 DETECTING DAMAGES OUT OF LIMIT IN BOTH NOSE LANDING GEAR
- [SDR ASMF201009001](https://openairdocs.org/sdr/ASMF201009001.md): Skin · damaged · Sep 1, 2010 · N774AM · Boeing 7772Q8 · Fuselage Main, Plate/Skin
  > CAPTAIN REPORTED A LIGHTNING STRIKE IN THE LT SIDE LOWER FUSELAGE SKIN. MX PERFORMED A LIGHTNING STRIKE INSPECTION IAW MM 05-51-19, NO DAMAGES WERE DETECTED.
- [SDR ASMF201008002](https://openairdocs.org/sdr/ASMF201008002.md): Pressure Sensor · damaged · Aug 24, 2010 · N746AM · Boeing 7772Q8 · Engine Oil Pressure
  > ACFT RETURNED OF FLIGHT DUE TO DURING CLIMB, EICAS MESSAGE AND LIGHT TURNED ON OF ENG OIL FILTER L WAS SHOWN. THE FLIGHT CREW PERFORMED THE QRH ENG OIL FILTER L, R PROCEDURE, CONFIRMING THE FAILURE. MX PERSONNEL REPLACED THE LT OIL DIFFERENTIAL PRESSURE SENSOR
- [SDR ASMF201008001](https://openairdocs.org/sdr/ASMF201008001.md): Tire · detached · Aug 19, 2010 · N745AM · Boeing 7772Q8 · Tire
  > DURING TAKEOFF RUN; A STRONG NOISE WAS HEARD, IECAS MESSAGE OF TIRE PRESS WAS SHOWN AND TIRE PRESS LIGHT TURNED ON, THE TIRE NR 1 WAS DEFLATED AND THE FLIGHT CONTINUED TO MAD IAW FCT 777 (TM) 8.18 (32-40-72-00 PROCEDURE). MX DETECTED MAIN TIRE NR 1 FLOOR DETA

Next page: https://openairdocs.org/model/boeing-777-2q8/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 aircraft_model_key = '7772Q8'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/boeing-777-2q8/reports

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