# Service difficulty reports: N817AL, cancelled Nov 16, 2010 A list on [N817AL, cancelled Nov 16, 2010](https://openairdocs.org/deregistered/N817AL-2010-11-16.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 3 · 117 reports - [SDR TSAA0753060](https://openairdocs.org/sdr/TSAA0753060.md): Skin · cracked · Oct 28, 2007 · N817AL · Boeing 7372X6C · Fuselage Main, Plate/Skin > IN THE PROCESS OF ECO 3512, NDT INSPECTION DISCOVERED THE AFT CARGO DOOR CUTOUT AFT FRAME CRACKED. REPLACED THE FRAME IN ACCORDANCE WITH ECO 3512. - [SDR TSAA0628053](https://openairdocs.org/sdr/TSAA0628053.md): Pump · malfunctioned · Jul 12, 2006 · N817AL · Boeing 7372X6C · Fuel Boost Pump > AFTER LEVELING OFF AT 21,000 FEET, THE NR 2 FORWARD FUEL BOOST PUMP LIGHT BEGAN FLICKERING ON AND OFF. THE CREW REVIEWED THEIR QRH AND CONTACTED MAINTENANCE CONTROL. MAINTENANCE CONTROL ADVISED THE CREW TO RETURN TO HNL DUE TO NO MAINTENANCE PERSONNEL IN HIL - [SDR TSAA0577041](https://openairdocs.org/sdr/TSAA0577041.md): Line · obstructed · Sep 19, 2005 · N817AL · Boeing 7372X6C · Engine Indicating System > CARGO FLT 820 HNL-OGG. AT CRUISE, CREW NOTED NR 1 ENGINE EPR 0.30 LESS THAN NR 2 ENGINE. N1 AND N2 SAME ON BOTH ENGINES. CREW RETURNED TO HNL WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED DEBRIS FROM THE NR 1 PT2 SENSE LINE PER AMM 72-00-00 AND RETURNED TH - [SDR TSAA0577033](https://openairdocs.org/sdr/TSAA0577033.md): Transmitter · defective · Jul 27, 2005 · N817AL · Boeing 7372X6C · Engine Pressure Ratio (EPR) > FLT 850 HNL - ITO. ON TAKEOFF, NUMBER 1 ENGINE PRESSURE RATIO INDICATION STOPPED INCREASING AT 170 WHILE THE NUMBER 2 ENGINE INDICATION OPERATED NORMALLY. CREW ABORTED TAKEOFF AT 80 KNOTS. AIRCRAFT RETURNED TO GATE WITHOUT FURTHER INCIDENT. MAINTENANCE REP - [SDR TSAA0475073](https://openairdocs.org/sdr/TSAA0475073.md): Line · loose · Sep 29, 2004 · N817AL · Boeing 7372X6C · Engine Bleed Air System > NR 1 ENGINE WILL NOT REACH TAKEOFF POWER; REPORTED BY CREW. MAINTENANCE TROUBLE SHOOTING FOUND THE AFT PT7 LINE LOOSE. SECURED THE LINE; RAN ENGINE TO POWER. ALL PARAMETERS, OPS AND LEAK CHECK GOOD. SYSTEM CHECK OK. AIRCRAFT RETURNED TO SERVICE. - [SDR TSAA0475050](https://openairdocs.org/sdr/TSAA0475050.md): Duct · failed · Jun 28, 2004 · N817AL · Boeing 7372X6C · Engine Bleed Air System > DURING CLIMB-OUT, THE NR 2 ENGINE OVERHEAT LIGHT CAME ON. RETURNED TO HNL. REMOVED AND REPLACED THE NR 2 ENGINE NOSE-COWL ANTI-ICE DUCT DUE TO LEAK AT THE BELLOWS. LEAK CHECK OK, AIRCRAFT RETURNED TO SERVICE. - [SDR TSAA0434049](https://openairdocs.org/sdr/TSAA0434049.md): Indicator · failed · Jun 21, 2004 · N817AL · Boeing 7372X6C · Rate of Climb Indicator > CAPTAINS VERTICAL SPEED INDICATOR INOPERATIVE. RETURN TO HNL. REPLACED VERTICAL SPEED INDICATOR, OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. - [SDR TSAA0434043](https://openairdocs.org/sdr/TSAA0434043.md): Pitot Tube · contaminated · Jun 1, 2004 · N817AL · Boeing 7372X6C · Pitot/Static System > CAPTAINS AND FIRST OFFICERS AIRSPEED INDICATORS READ 20 KTS DIFFERENCE. RETURNED TO HNL. REMOVED FOD FROM PITOT TUBE, SYS OPS & LEAK CHECK GOOD IAW AMM 34-11-00. AIRCRAFT RETURNED TO SERVICE. - [SDR TSAA0353108](https://openairdocs.org/sdr/TSAA0353108.md): Skin · cracked · Apr 24, 2003 · N817AL · Boeing 7372X6C · Fuselage Main, Plate/Skin > TRIMMED OUT DAMAGED AREA. VERIFIED CRACK FREE USING HFEC INSPECTION. FABRICATED REPAIR DOUBLER FORM 2024-T3. ALODINED AND PRIMED ALL BARE SURFACES. INSTALLED REPAIR PARTS PER SRM 53-30-3, FIGURE 1. APPLIED FILLET SEAL WITH BMS 5-95 SEALANT AROUND EDGES OF - [SDR TSAA0353060](https://openairdocs.org/sdr/TSAA0353060.md): Skin · cracked · Apr 7, 2003 · N817AL · Boeing 7372X6C · Fuselage Main, Plate/Skin > CUT OUT DAMAGED AREA. VERIFIED CRACK FREE USING HFEC. FABRICATED REPAIR PLATE. ALODINED AND PRIMED ALL BARE SURFACES. INSTALLED REPAIR PARTS USING FASTENERS IDENTIFIED IN TABLE II. REPAIR COMPLETED IAW SRM 53-30-3, FIGURE 1. AIRCRAFT RETURNED TO SERVICE. - [SDR TSAA0333052](https://openairdocs.org/sdr/TSAA0333052.md): Battery Pack · discharged · Feb 13, 2003 · N817AL · Boeing 7372X6C · Emergency Lighting > REPLACED NR 2 FLOOR EMERGENCY LIGHT ASSEMBLY DUE TO LOW VOLTAGE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) - [SDR TSAA0249213](https://openairdocs.org/sdr/TSAA0249213.md): Apu · failed · Oct 17, 2002 · N817AL · Boeing 7372X6C · APU Core Engine > JUST AFTER TAKEOFF THE APU OVERSPEED LIGHT CAME ON AND THE APU SHUTDOWN. THE AIRCRAFT RETURNED AND LANDED, WITH NO FURTHER INCIDENT. REPLACED THE APU ACCESSORY UNIT AND THE THREE SPEED SWITCH. GROUND OPS CHECK GOOD AND AN OVERWEIGHT LANDING CHECK WAS COMPLE - [SDR TSAA0253202](https://openairdocs.org/sdr/TSAA0253202.md): Flap Track · damaged · Sep 25, 2002 · N817AL · Boeing 7372X6C · Trailing Edge Flaps > FLAP TRACK ATTACHMENT FITTING HOLE ELONGATED. REPAIRED AND AIRCRAFT RETURNED TO SERVICE. - [SDR TSAA0251192](https://openairdocs.org/sdr/TSAA0251192.md): Skin · cracked · Aug 26, 2002 · N817AL · Boeing 7372X6C · Fuselage Main, Plate/Skin > BS 380 STRING 15R CRACK ON FUS SKIN. HFEC INSP EDGES ON CUTOUT,.040 IN INSUR CUT, FAB 2024-T3, CLAD SHEET.032 IN FILLER,.050 IN FILLER, AND.050 DOUBLER, MAINTAINING 2D MIN EDGE MARGIN, 2.0 INCH MIN INSIDE CORNER AND.5 IN MIN OUTSIDE CORNER RADIUS WITH C - [SDR TSAA0277173](https://openairdocs.org/sdr/TSAA0277173.md): Transmitter · inoperative · Aug 11, 2002 · N817AL · Boeing 737200 · Engine Pressure Ratio (EPR) > NR 1 ENGINE EPR DROPPED OFF ON CLIMB OUT OF 7,000 FEET. NR 1 ENGINE EPR WAS 1.73 AND NR 2 ENGINE EPR WAS 1.85. BOTH THE NR 1 AND NR 2 ENGINES NR 1 WAS 89 PERCENT AND NR 2 WAS 92 PERCENT. THE AIRCRAFT RETURNED AND LANDED IN HNL WITH NO FURTHER INCIDENT. (ET - [SDR TSAA0271172](https://openairdocs.org/sdr/TSAA0271172.md): Line · obstructed · Aug 11, 2002 · N817AL · Boeing 7372X6C · Engine (Turbine/Turboprop) > DURING CLIMB THE NR 1 ENGINE EGT INDICATED 600 DEGREES C WITH THRUST LEVER 4 INCHES AHEAD OF THE NR 2 ENGINE THRUST LEVER. THE NR 1 ENGINE EPR WAS 1.73 AND THE NR 2 ENGINE EPR WAS 1.83. THE FLIGHT RETURNED AND LANDED WITH NO FURTHER INCIDENT. (ETOPS A/C ON N - [SDR TSAA0253164](https://openairdocs.org/sdr/TSAA0253164.md): Skin · cracked · Jul 8, 2002 · N817AL · Boeing 7372X6C · Fuselage Main, Plate/Skin > IDENTIFIED A TWO AND A HALF INCH CRACK ON FUSELAGE SKIN AT BS 942 STRINGER 24R. TRIMMED OUT DAMAGED SKIN, HFEC EDGE OF TRIMMED AREA WITH NO DEFECTS NOTED, FABRICATED TWO EACH FILLER AND TWO EACH DOUBLER. INSTALLED REPAIR PARTS IAW SRM. AIRCRAFT RETURNED TO - [SDR TSAA0253163](https://openairdocs.org/sdr/TSAA0253163.md): Skin · cracked · Jul 8, 2002 · N817AL · Boeing 7372X6C · Fuselage Main, Plate/Skin > IDENTIFIED A TWO INCH CRACK ON FUSELAGE SKIN AT BS962 STRINGER 21L. TRIMMED OUT DAMAGED SKIN, HFEC EDGE OF TRIMMED AREA WITH NO DEFECTS NOTED, FABRICATED A FILLER AND DOUBLER. INSTALLED REPAIR PARTS IAW SRM. AIRCRAFT RETURNED TO SERVICE. - [SDR TSAA0253162](https://openairdocs.org/sdr/TSAA0253162.md): Skin · cracked · Jul 8, 2002 · N817AL · Boeing 7372X6C · Fuselage Main, Plate/Skin > IDENTIFIED ONE INCH CRACK ON FUSELAGE SKIN AT BS 277 STRINGER 11L. TRIMMED OUT DAMAGED SKIN, HFEC EDGE OF TRIMMED AREA WITH NO DEFECTS NOTED, FABRICATED A FILLER AND DOUBLER. INSTALLED REPAIR PARTS IAW SRM. AIRCRAFT RETURNED TO SERVICE. - [SDR TSAA0253161](https://openairdocs.org/sdr/TSAA0253161.md): Skin · cracked · Jul 8, 2002 · N817AL · Boeing 7372X6C · Fuselage Main, Plate/Skin > IDENTIFIED A TWO INCH CRACK ON FUSELAGE SKIN AT BS274 STRINGER 15R. TRIMMED OUT DAMAGED SKIN, HFEC EDGE OF TRIMMED AREA WITH NO DEFECTS NOTED, FABRICATED FILLER AND DOUBLER. INSTALLED REPAIR PARTS IAW SRM. AIRCRAFT RETURNED TO SERVICE. - [SDR TSAA0233154](https://openairdocs.org/sdr/TSAA0233154.md): Light · damaged · Jun 29, 2002 · N817AL · Boeing 7372X6C · Emergency Lighting > REPLACED FORWARD ENTRY DOOR IDENTIFIER LIGHT ASSEMBLY DUE TO DAMAGE. OPS CHECK, OK. AIRCRAFT RETURNED TO SERVICE. - [SDR TSAA0233153](https://openairdocs.org/sdr/TSAA0233153.md): Battery Pack · discharged · Jun 29, 2002 · N817AL · Boeing 7372X6C · Emergency Lighting > REPLACED FORWARD ENTRY DOOR IDENTIFIER POWER PACK DUE TO LOW VOLTAGE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. - [SDR TSA2002F00000](https://openairdocs.org/sdr/TSA2002F00000.md): Wire Harness · worn · Jun 19, 2002 · N817AL · Boeing 7372X6C · APU System Wiring > ENROUTE, THE APU SHUTDOWN DUE TO AN OVERSPEED. THE AIRCRAFT RETURNED WITHOUT FURTHER INCIDENT. MAINTENANCE RESTARTED THE APU AND CONDUCTED AN OPERATIONAL CHECK OF THE UNIT. THE OPERATIONAL CHECK WAS GOOD AND AN OVERWEIGHT LANDING INSPECTION WAS COMPLETED. - [SDR TSAA0233044](https://openairdocs.org/sdr/TSAA0233044.md): Battery Pack · inoperative · Feb 14, 2002 · N817AL · Boeing 7372X6C · Emergency Lighting > REPLACED NR 2 FLOOR PATH EMERGENCY EXIT LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) - [SDR TSAA0133171](https://openairdocs.org/sdr/TSAA0133171.md): Battery Pack · discharged · Dec 2, 2001 · N817AL · Boeing 7372X6C · Emergency Lighting > REPLACED NR 2 FLOOR PROXIMATELY EMERGENCY LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) - [SDR TSAA0153154](https://openairdocs.org/sdr/TSAA0153154.md): Skin · corroded · Nov 15, 2001 · N817AL · Boeing 7372X6C · Fuselage Main, Plate/Skin > DISCOVERED BULGING AT BS 1088, S-20R FUSELAGE SKIN. REMOVED THE CORRODED PORTION OF THE STRAP, FABRICATED AND INSTALLED REPAIR DOUBLER AND TRIPLER. RECEIVED 8110-3 APPROVAL. AIRCRAFT RETURNED TO SERVICE. (M) - [SDR TSAA0153157](https://openairdocs.org/sdr/TSAA0153157.md): Window Frame · cracked · Nov 14, 2001 · N817AL · Boeing 7372X6C · Fuselage Main, Structure > PERFORMED WINDOW CORNER FASTENER HOLE INSPECTION PER S/B 737-53A1177R6 AND DISCOVERED DEFECTS IN NUMEROUS AREAS AT LT FUSELAGE WINDOW CORNERS; 2 BETWEEN BS 500-520 AND 33 BETWEEN BS 727-907, RT FUSELAGE WINDOW CORNERS; 8 BETWEEN BS 360-540 AND 1 AT BS 727A-727 - [SDR TSAA0157155](https://openairdocs.org/sdr/TSAA0157155.md): Skin · corroded · Nov 9, 2001 · N817AL · Boeing 7372X6C · Wing, Plate/Skin > DISCOVERED CORROSION ON LEFT LOWER WING SURFACE, WS 500. REMOVED CORROSION, CONFIRMED REMOVAL OF CORROSION, FLAP PEENED REWORKED AREAS PER SOPM 20-10-03. AIRCRAFT RETURNED TO SERVICE. (M) - [SDR TSAA0157156](https://openairdocs.org/sdr/TSAA0157156.md): Skin · corroded · Nov 7, 2001 · N817AL · Boeing 7372X6C · Wing, Plate/Skin > DISCOVERED CORROSION AT LEFT LOWER WING SURFACE, WS 515.5. REMOVED CORROSION, CONFIRMED REMOVAL OF CORROSION, FLAP PEENED REWORKED AREAS PER SOPM 20-10-03. AIRCRAFT RETURNED TO SERVICE. (M) - [SDR TSAA0179120](https://openairdocs.org/sdr/TSAA0179120.md): Pressure Switch · faulty · Sep 28, 2001 · N817AL · Boeing 7372X6C · Engine Oil Pressure > FLT 953 - ITO-HNL - DURING A NON-ETOPS QC CARGO FLIGHT, THE NR 1 ENGINE OIL FILTER BYPASS LIGHT CAME ON. SHUTDOWN THE NR 1 ENGINE AND DECLARED AN EMERGENCY. UNEVENTFUL LANDING AT HNL. REMOVED AND REPLACED THE OIL BYPASS SWITCH IAW MM 79-35-011-4. INSPECTED - [SDR TSAA0133114](https://openairdocs.org/sdr/TSAA0133114.md): Battery Pack · discharged · Aug 31, 2001 · N817AL · Boeing 7372X6C · Emergency Lighting > REPLACED NR 1 FLOOR EMERGENCY LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) - [SDR TSAA0133094](https://openairdocs.org/sdr/TSAA0133094.md): Battery Pack · inoperative · Jul 20, 2001 · N817AL · Boeing 7372X6C · Lighting System > REPLACED NR 1 FLOOR EMERGENCY LGIHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) - [SDR TSAA0124078](https://openairdocs.org/sdr/TSAA0124078.md): Csd · failed · Jun 20, 2001 · N817AL · Boeing 7372X6C · Alternator-Generator Drive > FLT 915 - HNL-LIH - DURING FLIGHT, THE LOW OIL PRESSURE LIGHT CAME ON AND THE NR 1 ENGINE CSD GENERATOR WAS DISCONNECTED AQ MAINTENANCE WAS CONTACTED AND ADVISED PILOT TO RETURN TO HNL. AIRCRAFT RETURNED TO HNL AND BLOCKED IN T 0154 HOURS WITH NO FURTHER INC - [SDR TSAA0153057](https://openairdocs.org/sdr/TSAA0153057.md): Skin · damaged · May 8, 2001 · N817AL · Boeing 7372X6C · Fuselage Main, Plate/Skin > FUSELAGE SKIN WRINKLE BETWEEN BS 663.75 AND BS 706, S13 AND S16. (M) - [SDR TSAA0153058](https://openairdocs.org/sdr/TSAA0153058.md): Skin · damaged · May 8, 2001 · N817AL · Boeing 7372X6C · Fuselage Main, Plate/Skin > FOUND FUSELAGE SKIN WRINKLE BETWEEN BS 663.75 AND BS 706, S13L AND S16L. (M) - [SDR TSAA0153059](https://openairdocs.org/sdr/TSAA0153059.md): Frame · cracked · May 7, 2001 · N817AL · Boeing 7372X6C · Fuselage Main, Frame > FUSELAGE BS 727, STRINGER 18A LEFT OUTBOARD CHORD DETECTED CRACK BY METHOD OF HFEC INSPECTION. (M) - [SDR TSAA0153060](https://openairdocs.org/sdr/TSAA0153060.md): Frame · cracked · May 7, 2001 · N817AL · Boeing 7372X6C · Fuselage Main, Frame > FOUND FUSELAGE BS 727, STRINGER 18A RIGHT OUTBOARD CHORD DETECTED CRACK BY METHOD OF HFEC INSPECTION. (M) - [SDR TSAA0153061](https://openairdocs.org/sdr/TSAA0153061.md): Pressure Panel · cracked · May 1, 2001 · N817AL · Boeing 7372X6C · Fuselage Main, Bulkhead > FOUND CRACK NOTED AT LEFT UPPER CORNER NLG PRESSURE PANEL. CONFIRMED CRACK BY UTILIZING HFEC METHOD. (M) - [SDR TSAA0153062](https://openairdocs.org/sdr/TSAA0153062.md): Skin · cracked · May 1, 2001 · N817AL · Boeing 7372X6C · Fuselage Main, Plate/Skin > DURING HARD LANDING INSPECTION, DISCOVERED 2 INCHES CRACK AT BS 540, STRINGER 1R AND 2R, VERIFIED BY USING HFEC. (M) - [SDR TSAA0133041](https://openairdocs.org/sdr/TSAA0133041.md): Battery Pack · discharged · Apr 21, 2001 · N817AL · Boeing 7372X6C · Emergency Lighting > REPLACED NR 2 FLOOR EMERGENCY LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) - [SDR TSAA0133029](https://openairdocs.org/sdr/TSAA0133029.md): Battery Pack · discharged · Mar 3, 2001 · N817AL · Boeing 7372X6C · Emergency Lighting > REPLACED NR 1 AND NR 3 EMERGENCY FLOOR LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) - [SDR TSAA0152018](https://openairdocs.org/sdr/TSAA0152018.md): Door · cracked · Feb 18, 2001 · N817AL · Boeing 7372X6C · Cargo/Baggage Doors > IDENTIFIED CRACKS AT 3.25 INCH PROPAGATING FROM ONE RIVET TO ADJACENT RIVET ON MAIN CARGO DOOR AT BS 430, 2 INCHES BELOW STRINGER 14L CONFIRMED BY UTILIZING HFEC AND VISUAL METHOD. TRIM OUT THE CRACK DAMAGE, FABRICATED FILLERS FROM 2024-T3, FABRICATED EXTERNA - [SDR TSAA0033258](https://openairdocs.org/sdr/TSAA0033258.md): Battery Pack · discharged · Sep 3, 2000 · N817AL · Boeing 7372X6C · Emergency Lighting > REPLACED NR 4 FLOOR EMERGENCY LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) - [SDR TSAA0032192](https://openairdocs.org/sdr/TSAA0032192.md): Selector Valve · leaking · Aug 15, 2000 · N817AL · Boeing 7372X6C · Landing Gear Retraction/Extension System > FLT 248 - LIH-HNL - CLIMBING THROUGH 10,000 FT, BOTH MAIN GEAR RED AND GREEN LIGHTS ILLUMINATED WITH THE LANDING GEAR HANDLE IN THE OFF POSITION. AFTER REVIEWING THE ISSUE, THE LANDING GEAR HANDLE WAS PLACED TO DOWN AND ALL THREE GEARS INDICATED DOWN AND LOCK - [SDR TSAA0033183](https://openairdocs.org/sdr/TSAA0033183.md): Battery Pack · inoperative · Aug 1, 2000 · N817AL · Boeing 7372X6C · Lighting System > REPLACED NR 2 FLOOR EMERGENCY LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) - [SDR TSAA0033176](https://openairdocs.org/sdr/TSAA0033176.md): Battery Pack · inoperative · Jun 23, 2000 · N817AL · Boeing 7372X6C · Emergency Lighting > REPLACED NR 6 FLOOR EMERGENCY LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) - [SDR TSAA0033156](https://openairdocs.org/sdr/TSAA0033156.md): Light · inoperative · Jun 23, 2000 · N817AL · Boeing 7372X6C · Emergency Lighting > REPLACED NR 3 FLOOR EMERGENCY LIGHT BATTERY PACK. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) - [SDR TSAA0053158](https://openairdocs.org/sdr/TSAA0053158.md): Door Frame · damaged · May 25, 2000 · N817AL · Boeing 7372X6C · Fuselage Miscellaneous Structure > REPAIRED MAIN CARGO DOOR CUTOUT FRAME LEFT SIDE STATION 500, WBL 264.5 BY BLENDOUT OF ELONGATED FRAME HOLE IAW ECO 3145. AIRCRAFT RETURNED TO SERVICE. (M) - [SDR TSAA0027157](https://openairdocs.org/sdr/TSAA0027157.md): Skin · corroded · May 23, 2000 · N817AL · Boeing 7372X6C · Ailerons > REPAIRED RIGHT AILERON CONTROL QUADRANT AT WING STATION 519 BY BLENDOUT AND TREATING CORROSION IAW ECO 3147. AIRCRAFT RETURNED TO SERVICE. (M) - [SDR TSAA0033124](https://openairdocs.org/sdr/TSAA0033124.md): Battery Pack · inoperative · Apr 24, 2000 · N817AL · Boeing 7372X6C · Emergency Lighting > REPLACED FORWARD EXIT IDENTIFIER POWER PACK. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) Next page: https://openairdocs.org/deregistered/N817AL-2010-11-16/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 = 'N817AL' AND deregistration_id = 'N817AL-2010-11-16' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N817AL-2010-11-16/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.