# Service difficulty reports: N841AL, cancelled Oct 8, 2014

A list on [N841AL, cancelled Oct 8, 2014](https://openairdocs.org/deregistered/N841AL-2014-10-08.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

- [SDR TSAA20140113001](https://openairdocs.org/sdr/TSAA20140113001.md): Structure · corroded · Jan 9, 2014 · N841AL · Boeing 7372X6C · Horizontal Stabilizer Miscellaneous Structure
  > DURING A SCHEDULED A CHECK INSPECTION, AN AREA CORROSION DAMAGE 1.25 INCHES WIDE & 0.875 INCHES LONG & 0.060 INCHES DEEP WAS FOUND ON THE LT STABILIZER AT ELEVATOR STATION 102.5. REMOVED CORROSION, SANDED, POLISHED, BLENDED, REWORKED AREA & APPLIED A DOUBLER
- [SDR TSAA20130110001](https://openairdocs.org/sdr/TSAA20130110001.md): Skin · cracked · Jan 10, 2013 · N841AL · Boeing 7372X6C · Fuselage Main, Plate/Skin
  > DURING SERVICE CHECK FOUND AN APPROX 2" CRACK ON THE LT SIDE FUSELAGE AT BS 802, ABOVE STRINGER 18L. REPAIRED IAW SRM 53-30-3, FIG. 48.
- [SDR TSAA20121001005](https://openairdocs.org/sdr/TSAA20121001005.md): Skin · cracked · Oct 1, 2012 · N841AL · Boeing 7372X6C · Fuselage Main, Plate/Skin
  > DURING SERVICE CHECK, FOUND AN APPROXIMATELY 2 INCH CRACK ON THE LT SIDE FUSELAGE AT BS 887, ABOVE STRINGER 17L. REPAIRED CRACK IAW SRM 53-30-3, FIG 48, DETAIL XI.
- [SDR 7AHR201205252279](https://openairdocs.org/sdr/7AHR201205252279.md): Stringer Clip · cracked · May 25, 2012 · N841AL · Boeing 7372X6C · Fuselage Main, Attach Fittings
  > STRINGER CLIP CRACKED AT FUSELAGE BS 277 AT STRINGER 15R. REMOVED DAMAGED STRINGER CLIP IAW SRM 51-30-02. FABRICATED NEW STRINGER CLIP IAW SRM 51-30-06. INSTALLED NEW STRINGER CLIP IAW SRM 51-30-2.
- [SDR 7AHR201205252294](https://openairdocs.org/sdr/7AHR201205252294.md): Skin · corroded · May 25, 2012 · N841AL · Boeing 7372X6C · Horizontal Stabilizer, Plate/Skin
  > LT HORIZONTAL STABILIZER UPPER SURFACE REAR SPAR HAS A BROKEN RIVET HEAD AND A BULGE IN SKIN AROUND BROKEN RIVET AT STABILIZER STATION 66.5. REMOVED T/E SKIN FASTENERS. DISCOVERED CORROSION AROUND AFT SPAR OF HORIZONTAL STABILIZER. REMOVED CORROSION ON AFT S
- [SDR 7AHR201205252210](https://openairdocs.org/sdr/7AHR201205252210.md): Stringer Splice · corroded · May 25, 2012 · N841AL · Boeing 7372X6C · Fuselage Main, Longeron/Stringer
  > CORROSION ON STRINGER SPLICE AT STA 907 AT STRINGER 26L. FOUND STRINGER SPLICE TO BE EXFOLIATED OUT OF LIMITS. REMOVED STRINGER SPLICE IAW SRM 51-30-2. FABRICATED STRINGER SPLICE FILLER MATERIAL IAW SRM 53-10-3 AND INSTALLED REPAIR PARTS IAW SRM 51-30-2.
- [SDR 7AHR201205252424](https://openairdocs.org/sdr/7AHR201205252424.md): Floorbeam · corroded · May 25, 2012 · N841AL · Boeing 7372X6C · Fuselage Main, Floor Beam
  > CORROSION ON FLOORBEAM AT STA 787 AND RBL 40 THROUGH 55. REMOVED CORROSION IAW SRM 51-30-2. FABRICATED FLOORBEAM REPAIR IAW ECO 53-04407-1. INSTALLED FABRICATED FLOORBEAM IAW DWG 53-04407-1.
- [SDR 7AHR201205242306](https://openairdocs.org/sdr/7AHR201205242306.md): Plate · gouged · May 24, 2012 · N841AL · Boeing 7372X6C · Nacelle/Pylon, Main Frame
  > NR 2 ENGINE CROSSBEAM LOWER INBD ENGINE TO WING FAIRING HAS GOUGES ON CROSSBEAM FACE. REMOVED DAMAGED PLATE FROM CROSSBEAM IAW 51-30-2. FABRICATED NEW PLATE IAW SRM 51-20-1. INSTALLED NEW PLATE ON CROSSBEAM FACE SRM 51-30-2.
- [SDR 7AHR201205242207](https://openairdocs.org/sdr/7AHR201205242207.md): Stringer · corroded · May 24, 2012 · N841AL · Boeing 7372X6C · Fuselage Main, Longeron/Stringer
  > CORROSION AT BS 1016 AT AFT PRESSURE BULKHEAD AT STRINGER 24L. REMOVED STRINGER END FITTING AND ALSO FOUND END OF STRINGER WAS ALSO CORRODED. FABRICATED NEW STINGER END FITTING AND STRINGER SPLICE, ALL REPAIR PARTS INSTALLED IAW SRM 53-10-3.
- [SDR 7AHR201205242213](https://openairdocs.org/sdr/7AHR201205242213.md): Support · crushed · May 24, 2012 · N841AL · Boeing 7372X6C · Fuselage Miscellaneous Structure
  > BS 727 AT STRINGER 19R HORIZONTAL BULKHEAD PANEL SUPPORT FRAME IS CRUSHED IN AFT PIT. REMOVED HORIZONTAL BULKHEAD PANEL SUPPORT FRAME AT FUSELAGE STATION 727 IAW SRM 51-30-2. FABRICATED NEW SUPPORT FERAME IAW SRM 51-20-01. INSTALLED NEW SUPPORT FRAME IAW SRM
- [SDR 7AHR201205292272](https://openairdocs.org/sdr/7AHR201205292272.md): Shear Tie · corroded · May 24, 2012 · N841AL · Boeing 7372X6C · Fuselage Internal Mounting Structure
  > CORROSION AT FUSELAGE STA 400 AND STRINGER 26R, FUSELAGE FRAME. REMOVED CORRORED SHEAR TIE IAW SRM 51-30-02, FABRICATED AND ISTALLED A NEW SHEAR TIE IAW SRM 51-10-02 AND 51-30-02.
- [SDR 7AHR201205222468](https://openairdocs.org/sdr/7AHR201205222468.md): Fairing · damaged · May 22, 2012 · N841AL · Boeing 7372X6C · Trailing Edge Flaps
  > NR 3 FLAP FAIRING FORWARD LOWER L/E IS DAMAGED. REPAIRED IAW SRM`S 51-30-2, & 51-40-3.
- [SDR 7AHR201205222209](https://openairdocs.org/sdr/7AHR201205222209.md): Stringer Splice · corroded · May 22, 2012 · N841AL · Boeing 7372X6C · Fuselage Main, Longeron/Stringer
  > CORROSION AT FUSELAGE STA 907 AT STR 27L AT STRINGER SPLICE. REMOVED STRINGER SPLICE AND STRINGER CLIP DUE TO CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 51-30-02. FABRICATED REPAIR COMPONENTS IAW SRM 53-10-03. INSTALLED REPAIR COMPONENTS IAW SRM 51-30-02.
- [SDR 7AHR201205222466](https://openairdocs.org/sdr/7AHR201205222466.md): Frame · corroded · May 22, 2012 · N841AL · Boeing 7372X6C · Fuselage Main, Structure
  > AFT TAIL CONE ACCESS DOOR PANEL NR 3802 FRAME HAS CORRODED RIVET HEADS AND RUB PADS. REMOVED RIVETS AND RUB PADS FROM TAIL CONE ACCESS DOOR IAW SRM 51-30-2. FABRICATED NEW RUB PADS AND INSTALLED RUB PADS AND NEW FASTENERS AS IAW SRM 51-30-2.
- [SDR 7AHR201205222074](https://openairdocs.org/sdr/7AHR201205222074.md): Skin · misrepaired · May 22, 2012 · N841AL · Boeing 7372X6C · Fuselage Main, Plate/Skin
  > LOWER FUSELAGE PRESSURIZATION LEAK AT EXTERNAL REPAIR FWD EDGE AT STA 907 AT STRINGER 20L AT LAP SEAM AND BUTT SPLICE DOWN TO STR 25L LAP SEAM. REMOVED FASTENERS IN EXISTING REPAIR AT STR 20L STA 907 - 917. REAMED HOLES TO PROPER SIZE IAW SRM 51-30-05, FIG 3
- [SDR 7AHR38412A2073](https://openairdocs.org/sdr/7AHR38412A2073.md): Skin · misrepaired · May 22, 2012 · N841AL · Boeing 7372X6C · Fuselage Main, Plate/Skin
  > LOWER FUSELAGE, PRESSURIZATION LEAK AT EXTERNAL REPAIR (APPROX 30 RIVETS) BELOW R-1 DOOR. STA 312 AT STRINGER 19R LAP SEAM. REMOVED FASTENERS AT LOWER FUSELAGE AT STA 312 STR 19R AT LAP SEAM. PERFORMED NDT INSP OF FASTENER HOLES, NO DEFECT NOTED. FOUND WHEN
- [SDR TSAA1153010](https://openairdocs.org/sdr/TSAA1153010.md): Skin · cracked · Aug 24, 2011 · N841AL · Boeing 7372X6C · Fuselage Main, Plate/Skin
  > DURING SERVICE CHECK, FOUND A 2 INCH CRACK ON THE RT SIDE FUSELAGE AT BS 360+5.5, ABOVE STRINGER 15R. THE CRACK WAS REPAIRED IN ACCORDANCE WITH ECO 3826, SB 737-53A1177 REVISION 6 & SRM 53-30-03 FIGURE 48.
- [SDR TSAA1153005](https://openairdocs.org/sdr/TSAA1153005.md): Skin · cracked · Apr 10, 2011 · N841AL · Boeing 7372X6C · Fuselage Main, Plate/Skin
  > DURING THE DAILY SERVICE CHECK, A 2 IN CRACK AT BODY STA 259.5, 1 IN ABOVE STRINGER 16R WAS DISCOVERED DURING THE VISUAL CHECK OF THE FUSELAGE. THE CRACK WAS CONFIRMED WITH HFEC INSP AND WAS REPAIRED IAW SRM 53-30-3, FIG 48 DETAIL VIII. THE ACFT WAS RETURNED
- [SDR TSAA1156003](https://openairdocs.org/sdr/TSAA1156003.md): Window · cracked · Apr 3, 2011 · N841AL · Boeing 7372X6C · Flight Compartment Windows
  > NON-ETOPS FLIGHT 54 HNL-ITO. ON DESCENT, THE CAPTAIN’S NR 2 WINDOW OUTER PANE CRACKED. GLASS REMAINED INTACT AND THERE WAS NO LOSS OF PRESSURIZATION. CREW RETURNED TO DEPARTURE WITHOUT FURTHER INCIDENT. MX R & R THE CAPTAIN’S NR 2 WINDOW IAW AMM 56-12-11 AN
- [SDR TSAA1179002](https://openairdocs.org/sdr/TSAA1179002.md): Oil Filter · separated · Feb 18, 2011 · N841AL · Boeing 7372X6C · Turbine Engine Oil System
  > FLT 40. AFTER ADVANCING THE THROTTLES THE CREW NOTED THE NR 2 ENGINE LOW OIL PRESSURE LIGHT ILLUMINATE FOLLOWED BY A DECREASE IN NR 2 ENGINE OIL QUANTITY. THE CREW ABORTED THE TAKE-OFF AND SHUTDOWN THE NR 2 ENGINE AND RETURNED TO THE CARGO RAMP. MAINTENANCE
- [SDR TSAA1027019](https://openairdocs.org/sdr/TSAA1027019.md): Indicator · failed · Nov 16, 2010 · N841AL · Boeing 7372X6C · Trailing Flap Position Indicating System
  > DURING CLIMB, THE CREW SELECTED FLAPS UP AND NOTED A SPLIT-FLAP INDICATION, WITH NO ROLL ENCOUNTERED. CREW ATTEMPTED TO SELECT FLAPS 1 WITH NO EFFECT. CREW DECLARED AN EMERGENCY, ACCOMPLISHED T/E FLAPS DISAGREE CHECK LIST WITH FLAPS 15. ACFT LANDED WITHOUT
- [SDR EE4Y100357](https://openairdocs.org/sdr/EE4Y100357.md): Structure · corroded · Aug 19, 2010 · N841AL · Boeing 7372X6C · Fuselage Main, Bulkhead
  > FWD CARGO COMPARTMENT BULKHEAD BS 540 BTWN STR 22L AND 23L CHORD HORIZ FLANGE WITH CORROSION (THE CORROSION REQUIRES A MAJOR REPAIR).
- [SDR EE4Y100340](https://openairdocs.org/sdr/EE4Y100340.md): Stringer · cracked · Aug 17, 2010 · N841AL · Boeing 7372X6C · Fuselage Main, Longeron/Stringer
  > TAIL COMPARTMENT, STA 1132, STRINGER 5 RIGHT WITH CRACK. THE CRACK REQUIRES A MAJOR REPAIR.
- [SDR EE4Y100339](https://openairdocs.org/sdr/EE4Y100339.md): Stringer · cracked · Aug 17, 2010 · N841AL · Boeing 7372X6C · Fuselage Main, Longeron/Stringer
  > TAIL COMPARTMENT STA 1132 STRINGER 5 LT WITH CRACK. THE CRACK REQUIRES A MAJOR REPAIR.
- [SDR EE4Y100338](https://openairdocs.org/sdr/EE4Y100338.md): Bulkhead · corroded · Aug 17, 2010 · N841AL · Boeing 7372X6C · Fuselage Main, Bulkhead
  > LOWER FUSELAGE, FWD CARGO COMPARTMENT, STA 540 BULKHEAD BETWEEN STRINGER 22 LT AND 23 LT CHORD HORIZONTAL FLANGE WITH CORROSION. THE CORROSION REQUIRES A MAJOR REPAIR.
- [SDR EE4Y100336](https://openairdocs.org/sdr/EE4Y100336.md): Floorbeam · corroded · Aug 13, 2010 · N841AL · Boeing 7372X6C · Fuselage Main, Floor Beam
  > UPPER FUSELAGE, FLOORBEAM LOWER FLANGE WITH CORROSION AT STA 847 BETWEEN RBL 42 AND RBL 59. THE CORROSION REQUIRES A MAJOR REPAIR.
- [SDR EE4Y100335](https://openairdocs.org/sdr/EE4Y100335.md): Floorbeam · corroded · Aug 13, 2010 · N841AL · Boeing 7372X6C · Fuselage Main, Floor Beam
  > UPPER FUSELAGE, FLOORBEAM LOWER FLANGE WITH CORROSION AT STA 867 BETWEEN RBL 26 AND RBL 56. THE CORROSION REQUIRES A MAJOR REPAIR.
- [SDR EE4Y100337](https://openairdocs.org/sdr/EE4Y100337.md): Floorbeam · corroded · Aug 13, 2010 · N841AL · Boeing 7372X6C · Fuselage Main, Floor Beam
  > UPPER FUSELAGE, FLOORBEAM WITH CORROSION AT UPPER FLANGE AT STA 344 BETWEEN LBL 43 & RBL 11. THE CORROSION REQUIRES MAJOR REPAIR.
- [SDR EE4Y100334](https://openairdocs.org/sdr/EE4Y100334.md): Bear Strap · cracked · Aug 12, 2010 · N841AL · Boeing 7372X6C · Fuselage Main, Plate/Skin
  > MAIN CARGO DOOR, FWD UPPER CORNER CUTOUT, FUSELAGE SKIN, BEAR STRAP WITH CRACK. THE CRACK REQUIRES A MAJOR REPAIR.
- [SDR EE4Y100333](https://openairdocs.org/sdr/EE4Y100333.md): Floorbeam · corroded · Aug 12, 2010 · N841AL · Boeing 7372X6C · Fuselage Main, Floor Beam
  > UPPER FUSELAGE, BS 787 FLOORBEAM, LOWER FLANGE CORRODED. THE DAMAGE REQUIRES A MAJOR REPAIR.
- [SDR EE4Y100332](https://openairdocs.org/sdr/EE4Y100332.md): Bulkhead · dented · Aug 11, 2010 · N841AL · Boeing 7372X6C · Fuselage Main, Bulkhead
  > FUSELAGE BULKHEAD BS 1016, AFT FACE, WEB DENTED AT WBL 166, RBL 7. THE DENT REQUIRES A MAJOR REPAIR.
- [SDR EE4Y100330](https://openairdocs.org/sdr/EE4Y100330.md): Bear Strap · cracked · Aug 11, 2010 · N841AL · Boeing 7372X6C · Fuselage Main, Plate/Skin
  > UPPER FUSELAGE, FWD ENTRY DOOR, LOWER HINGE CUTOUT AT BS 304.5 WL 235, INTERNAL BEAR STRAP WITH CRACK. THE CRACK REQUIRES MAJOR REPAIR.
- [SDR EE4Y100319](https://openairdocs.org/sdr/EE4Y100319.md): Spar · corroded · Aug 10, 2010 · N841AL · Boeing 7372X6C · Wing Spar
  > RIGHT WING LEADING EDGE FRONT SPAR LOWER CHORD WITH CORROSION ON LOWER FLANGE. THE CORROSION REQUIRES A MAJOR REPAIR.
- [SDR EE4Y100309](https://openairdocs.org/sdr/EE4Y100309.md): Skin Panel · dented · Aug 9, 2010 · N841AL · Boeing 7372X6C · Fuselage Main, Plate/Skin
  > LOWER EXTERNAL FUSELAGE AT BS 727A+6.25 BETWEEN STR 22R AND STR 23R SKIN WITH DENT. THE DENT REQUIRES MAJOR REPAIR.
- [SDR EE4Y100264](https://openairdocs.org/sdr/EE4Y100264.md): Skin Panel · dented · Aug 5, 2010 · N841AL · Boeing 7372X6C · Fuselage Main, Plate/Skin
  > LOWER FUSELAGE, AT BS 727+12.5 BETWEEN STRINGER 20 RT AND STRINGER 21 RT SKIN WITH DENT. THE DENT REQUIRES MAJOR REPAIR.
- [SDR TSAA1053008](https://openairdocs.org/sdr/TSAA1053008.md): Stringer · cracked · Apr 26, 2010 · N841AL · Boeing 7372X6C · Fuselage Main, Longeron/Stringer
  > DISCOVERED 1" CRACK DURING SCHEDULED INSP AT BS 492.4, S-22R (AFT SIDE OF FWD CARGO DOOR CUTOUT FWD END OF STRINGER). R & R STRINGER ASSY IAW SRM 53-10-3, FIG 1, APPLIED CORROSION INHIBITOR.
- [SDR TSAA1027006](https://openairdocs.org/sdr/TSAA1027006.md): Proximity Sensor · failed · Mar 17, 2010 · N841AL · Boeing 7372X6C · Leading Edge Slat Position Indicating System
  > DURING CLIMB, AFTER THE FLAPS WERE RETRACTED, THE FLIGHT CREW NOTED THE LE FLAPS TRANSIT ANNUNCIATOR REMAINED ILLUMINATED. CREW ACCOMPLISHED THE QRH PROCEDURES AND ELECTED TO RETURN TO DEPARTURE. THE ACFT LANDED WITHOUT ANY FURTHER INCIDENT. MX R & R THE NR
- [SDR TSAA1026002](https://openairdocs.org/sdr/TSAA1026002.md): Fire Detector · false activation · Jan 19, 2010 · N841AL · Boeing 7372X6C · Fire Detection
  > NON-ETOPS. DURING CLIMB THE CREW NOTED A FIRE INDICATION ON THE NR 2 ENG. CREW ACCOMPLISHED ALL RELATED QRH AND CHECKLIST PROCEDURES AND SHUTDOWN THE NR 2 ENGINE AND DISCHARGED ENGINE FIRE EXTINGUISHERS. CREW RETURNED TO DEPARTURE WITHOUT FURTHER INCIDENT.
- [SDR TSAA1077001](https://openairdocs.org/sdr/TSAA1077001.md): Duct · cracked · Jan 11, 2010 · N841AL · Boeing 7372X6C · Engine Bleed Air System
  > FLT NR 58 (HNL ITO)- ON CLIMB OUT, NR 1 ENG FIRE WARNING LIGHT STARTED TO FLICKER AND BELL STARTED TO RING. PULLED BACK TO IDLE CONTINUED TO FLY AT IDLE, LIGHT AND BELL WENT OUT. R & R NR1 NOSE COWL DUCT DUE TO CRACK. PERFORMED HIGH POWER ENGINE RUN LEAK AND
- [SDR TSAA0953011](https://openairdocs.org/sdr/TSAA0953011.md): Skin · cracked · Nov 23, 2009 · N841AL · Boeing 737282C · Fuselage Main, Plate/Skin
  > DURING SCHEDULED INSP A 3" CRACK WAS DISCOVERED AT BS 440, 450, S-16R FUSELAGE SKIN. REPAIRED SKIN BY REMOVING CRACK DEFECT, CONDUCTED HFEC INSP, ENLARGED TRIM BY 0.040" INSURANCE CUT, INSTALLED DOUBLER/ TRIPLER, MAINTAINED A 0.5" MIN. CORNER RADIUS, MAINTAIN
- [SDR TSAA0932009](https://openairdocs.org/sdr/TSAA0932009.md): Shutoff Valve · inoperative · Sep 2, 2009 · N841AL · Boeing 7372X6C · Landing Gear Brake System
  > ON TAXI-OUT, THE "ANTI-SKID INOP" LIGHT ILLUMINATED AND THE "FAIL WARN AND PARK BRAKE" CIRCUIT BREAKER POPPED. RETURNED TO RAMP. MX REMOVED AND REPLACED THE PARKING BRAKE SHUT OFF VALVE IAW MM 32-44-21. OPS AND LEAK CHECK OK. ACFT RETURNED TO SERVICE.
- [SDR TSAA0926005](https://openairdocs.org/sdr/TSAA0926005.md): Fire Loop · malfunctioned · Jun 26, 2009 · N841AL · Boeing 7372X6C · Fire Detection
  > FLT 42, ENG NR 1 (OVERHEAT WARN) LIGHT FLICKERING DURING TAXI. RETURNED TO BLOCK. TRIED FIRE CONTROL MODULE, FIRE DETECTION UNIT AND DISCONNECTED NR1 ENG FIREWALL CONNECTOR, LIGHT STILL FLICKERING. RE-INSTALLED ORIGINAL COMPONENTS AND CONNECTOR. REMOVED AND
- [SDR TSAA0879020](https://openairdocs.org/sdr/TSAA0879020.md): Transmitter · failed · Jun 10, 2008 · N841AL · Boeing 7372X6C · Engine Oil Quantity
  > FLIGHT 913 HNL-LIH. DURING TAKEOFF, THE NR 2 ENGINE OIL QUANTITY DECREASED. ELECTED TO ABORT TAKEOFF. INDICATIONS RETURNED TO NORMAL DURING ABORT; ALL ENGINE PARAMETERS WERE NORMAL. MX REMOVED AND REPLACED THE NR 2 ENGINE OIL QUANTITY TRANSMITTER. OPS AND
- [SDR TSAA0721065](https://openairdocs.org/sdr/TSAA0721065.md): Controller · malfunctioned · Dec 14, 2007 · N841AL · Boeing 7372X6C · Air Distribution System
  > FLIGHT 48 HNL-ITO - DURING CLIMB THE CREW NOTED THE RIGHT SUPPLY DUCT PRESSURE READING 100 PSI (FULL SCALE). THE CREW LANDED IN HNL WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LEFT RAM AIR DOOR CONTROL AND PERFORMED AN ENGINE RUN WITH ALL
- [SDR TSAA0731057](https://openairdocs.org/sdr/TSAA0731057.md): Fdau · failed · Oct 15, 2007 · N841AL · Boeing 7372X6C · Flight Management Computing Hardware System
  > NON-ETOPS FLIGHT 278 HNL-KOA, AT 5000 FT, THE CREW NOTED THE FLIGHT RECORDER OFF LIGHT ILLUMINATED. THE CREW RETURNED TO HNL WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE FLIGHT DATA ACQUISITION UNIT PER AMM 31-24-11 WITH ALL CHECKS SATISFAC
- [SDR TSAA0732044](https://openairdocs.org/sdr/TSAA0732044.md): Switch · failed · Aug 5, 2007 · N841AL · Boeing 7372X6C · Landing Gear System Wiring
  > NON-ETOPS FLIGHT 62 HNL - OGG - DURING CLIMB-OUT OF HNL, THE CREW REPORTED THE LANDING GEAR HANDLE STAYED IN THE DOWN POSITION WHEN THEY ATTEMPTED TO RAISE IT TO THE UP POSITION. THE CREW USED THE QRH PROCEDURES AND RAISED THE GEAR HANDLE USING THE OVER-RIDE

## 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 = 'N841AL' AND deregistration_id = 'N841AL-2014-10-08'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N841AL-2014-10-08/reports

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