# Service difficulty reports: N907HA, cancelled Sep 20, 2016

A list on [N907HA, cancelled Sep 20, 2016](https://openairdocs.org/deregistered/N907HA-2016-09-20.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 · 145 reports

- [SDR HNAA2014010300656](https://openairdocs.org/sdr/HNAA2014010300656.md): Bulb · inoperative · Jan 3, 2014 · N907HA · Dhav DHC8102 · Emergency Lighting
  > NR 1 EMERGENCY LIGHT IS INOPERATIVE. R & R BULB. OPS CHECKED GOOD.
- [SDR HNAA2013122500635](https://openairdocs.org/sdr/HNAA2013122500635.md): Bulb · inoperative · Dec 25, 2013 · N907HA · Dhav DHC8102 · Emergency Lighting
  > EMERGENCY CEILING LIGHT IS INOPERATIVE AT ROW 5DF. R & R EMERGENCY CEILING LIGHT BULB AT ROW 5DF. OPS CHECKED GOOD.
- [SDR HNAA2013121600617](https://openairdocs.org/sdr/HNAA2013121600617.md): Connector · dirty · Dec 16, 2013 · N907HA · Dhav DHC8102 · Flight Control System Wiring
  > RUDDER TRIM INOPERATIVE. INSPECTED AND CLEANED ACTUATOR CONNECTOR. OPS CHECKED GOOD.
- [SDR HNAA2013101100533](https://openairdocs.org/sdr/HNAA2013101100533.md): Hose · kinked · Oct 11, 2013 · N907HA · Dhav DHC8102 · Pitot/Static System
  > F/O`S ASI READS HIGHER THAN CAPTAIN'S AFTER TAKEOFF AND FOR DURATION OF FLIGHT IAW CHECKLIST. SWITCHED TO ALT SOURCE. NO FIX, FOUND RT PITOT HOSE KINKED. REPLACED HOSE. LEAK CHECKED PITOT SYS. OPS CHECKED GOOD IAW MM 34-11-11 AND 34-11-02.
- [SDR HNAA2013092000504](https://openairdocs.org/sdr/HNAA2013092000504.md): Wire · damaged · Sep 18, 2013 · N907HA · Dhav DHC8102 · Light System Wiring
  > -ESCAPE PATH EMERGENCY LIGHT BULB IS INOPERATIVE AT ROW 8. R & R LIGHT, AISLE MARKER DUE TO BAD WIRE CONNECTION.
- [SDR HNAA2013092000503](https://openairdocs.org/sdr/HNAA2013092000503.md): Bulb · dim · Sep 18, 2013 · N907HA · Dhav DHC8102 · Passenger Compartment Lighting
  > CABIN, CEILING EXIT SIGN AT CENTER ISLE OF ROW 1 IS DIM, R & R DIM LIGHTS OF CEILING EXIT SIGN AT CENTER ISLE OF ROW 1 OPS CHECKED GOOD, REINSTALLED CEILING COVER.
- [SDR HNAA2013080200441](https://openairdocs.org/sdr/HNAA2013080200441.md): Control Box · inoperative · Aug 2, 2013 · N907HA · Dhav DHC8102 · Engine Oil Quantity
  > NR 1 ENGINE OIL PRESSURE WARNING LIGHT ILLUMINATED CONTINUOUSLY ON CLIMB. OIL PRESSURE INDICATED NORMAL- IN GREEN ARC. ENGINE WAS SHUTDOWN IN FLIGHT. CREW REPORTED OIL/FUEL TEMPS NORMAL AND DID DECLARE AN EMERGENCY. CONNECTOR LIGHT REMAINS ON. JUMPED CONN
- [SDR HNAA2013072200417](https://openairdocs.org/sdr/HNAA2013072200417.md): Garlock Seal · damaged · Jul 22, 2013 · N907HA · Dhav DHC8102 · Hydraulic Handpump, Main
  > NR 1 OIL PRESSURE FLUCTUATED AND STEADILY FELL. FEATHERED NR 1 ENGINE AFTER PRESSURE FELL BELOW 55 PSI AND SHUTDOWN AFTER CONTINOUS ILLUMINATION OF CAUTION LIGHT. FOUND DRAIN LINE AT INBD IGNITER BAY CONNECTED TO PROP SHAFT DRAIN LEAKING. R & R PROP SHAFT SE
- [SDR HNAA2013072200416](https://openairdocs.org/sdr/HNAA2013072200416.md): Linkage · malfunctioned · Jul 22, 2013 · N907HA · Dhav DHC8102 · Drag Control System
  > PSCS SHOWS RT INBD SPOILER DEPLOYED. FOUND RT INBD SPOILER SYNCRO TRANSMITTER LINKAGE OVER CENTERED. REPOSITION AND CHECKED SECURITY. GROUND RAN AND OPS CHECKED GOOD.
- [SDR HNAA2013071500409](https://openairdocs.org/sdr/HNAA2013071500409.md): Bulb · failed · Jul 15, 2013 · N907HA · Dhav DHC8102 · Emergency Lighting
  > ONE EMERGENCY FLOOR LIGHT IS INOPERATIVE AT ROW 9. R & R BULB AT ROW 9 EMERGENCY FLOOR PATH LIGHTING. OPS CHECKED GOOD.
- [SDR HNAA2013071000404](https://openairdocs.org/sdr/HNAA2013071000404.md): None · none · Jul 10, 2013 · N907HA · Dhav DHC8102 · Standard Practices/Structures
  > AISLE EMERGENCY LIGHT IS INOPERATIVE AT ROW 7. CYCLED SWITCH, FOUND LIGHT TO BE OPERATIONAL, OPS CHECKED GOOD.
- [SDR HNAA2013071000403](https://openairdocs.org/sdr/HNAA2013071000403.md): None · none · Jul 10, 2013 · N907HA · Dhav DHC8102 · Standard Practices/Structures
  > LEFT AFT EGRESS LIGHT BULB IS INOPERATIVE. CYCLED SWITCH, FOUND LIGHTS TO BE OPERATIONAL. OPS CHECKED GOOD.
- [SDR HNAA2013062600364](https://openairdocs.org/sdr/HNAA2013062600364.md): Pseu · malfunctioned · Jun 26, 2013 · N907HA · Dhav DHC8102 · Landing Gear Position and Warning
  > WOW CAUTION LIGHT ILLUMINATED ON LANDING ROLL FOR APPROX THREE SECONDS, THEN EXTINGUISHED. R & R PSEU IAW MM 32-61-50. CHECKED WOW SENSOR GAPS IAW MM 32-10-11.
- [SDR HNAA2013050100243](https://openairdocs.org/sdr/HNAA2013050100243.md): Wire · damaged · May 1, 2013 · N907HA · Dhav DHC8102 · Landing Gear System Wiring
  > RT MLG ALTERNATE INDICATION IS INOPERATIVE. FOUND BROKEN WIRE. INSTALLED ENVIRONMENTAL SPLICE IAW STANDARD PRACTICE. OPS CHECKED GOOD. OK FOR SERVICE. LAST NIGHT, MX R & R SPLICES 3261-E1, 3262-E2. REPLACED LED 3262-CR1 AND 3262-CR2. NO FIX. CHECKED RESISTA
- [SDR HNAA2013021900080](https://openairdocs.org/sdr/HNAA2013021900080.md): Relay · failed · Feb 19, 2013 · N907HA · Dhav DHC8102 · AC Power Distribution System
  > LT AC BUSS FAILURE IN FLIGHT WITH EMERGENCY LIGHTS FLICKERING. ALSO ASSOCIATED CAUTION LIGHTS ON. R & R 2421-S2 AND 2421-K2. RAN ENGINES FOR OVER 10 MINUTES. OPS CHECKED ALL AC POWER RELATED SYS. NO DISCREPENCIES NOTED AT THIS TIME.
- [SDR HNAA2013021500061](https://openairdocs.org/sdr/HNAA2013021500061.md): Bulb · failed · Feb 15, 2013 · N907HA · Dhav DHC8102 · Emergency Lighting
  > 12TH EMERGENCY FLOOR PATH LIGHT IS INOPERATIVE. R & R BULB FOR EMERGENCY FLOOR PATH LIGHT. OPS CHECKED GOOD.
- [SDR HNAA2013021500058](https://openairdocs.org/sdr/HNAA2013021500058.md): Unknown · warning light · Feb 15, 2013 · N907HA · Dhav DHC8102 · Electrical Power System
  > RT AC BUSS CAUTION LIGHT ILLUMINATED IN FLIGHT WITH ASSOCIATED CAUTION LIGHTS. PROBLEM OCCURED TWO MINUTES AFTER SELECTING PROP HEAT ON. ON PREVIOUS THREE LEGS, NO AC BUSS CAUTION LIGHT WITH PROP HEAT SELECTED OFF. R & R 2421-S2. R & R 2421-K2. RAN ENGINE
- [SDR HNAA2013021100046](https://openairdocs.org/sdr/HNAA2013021100046.md): Unknown · unknown · Feb 11, 2013 · N907HA · Dhav DHC8102 · Central Warning
  > ON CLIMB OUT, LT AC BUSS, LT TRU AND LT ELEVATOR HORN HEAT CAUTION LIGHTS ILLUMINATED. RETURN TO FIELD. INSPECTED BOTH 1 AND 2 ENGINES PROP BRUSH BLOCKS AND CLEANED CONNECTOR PLUGS AS WELL. INSPECTED BOTH ENGINES PROP HEATER LEADS. NO DEFECTS NOTED. GROUN
- [SDR HNAA2013021100045](https://openairdocs.org/sdr/HNAA2013021100045.md): Brush Block · saturated · Feb 11, 2013 · N907HA · Dhav DHC8102 · Ice/Rain Protection System Wiring
  > ON CLIMBOUT, RT AC BUSS, RT TRU AND RT ELEVATOR HORN HEAT CAUTION LIGHTS CAME ON. STAYED ON FOR ENTIRE FLIGHT. NR 2 BRUSH BLOCK WAS OILED SOAKED. R & R NR 2 PROP BRUSH BLOCK. OPS CHECKED GOOD. OPS CHECKED IAW WC 24-20-04Q. BUS CONTACTOR OPS CHECKED NORMAL
- [SDR HNAA2013021100043](https://openairdocs.org/sdr/HNAA2013021100043.md): Generator · inoperative · Feb 11, 2013 · N907HA · Dhav DHC8102 · AC Generator-Alternator
  > ON CLIMB OUT, RT AC BUSS, RT TRU AND RT ELEVATOR HORN HEAT CAUTION LIGHTS ILLUMINATED. ACFT WAS AIR TURNBACK. R & R NR 2 AC GENERATOR, GCU IAW WC 24-20-11R. OPS AND LEAK CHECKED GOOD.
- [SDR HNAA2013020400031](https://openairdocs.org/sdr/HNAA2013020400031.md): Connector · saturated · Feb 4, 2013 · N907HA · Dhav DHC8102 · Ice/Rain Protection System Wiring
  > DURING CRUISE FLIGHT AT 12K, SELECTED PROP HEAT ON AND RT AC BUSS FAULT OCCURED. INSPECTED BOTH PROP BRUSH BLOCKS, FOUND NR 2 PROP BRUSH BLOCK CONNECTOR PLUG SOAKED WITH DEICE FLUID. CLEANED AND DRIED CONNECTOR PLUG AS REQUIRED. GROUND RAN BOTH ENGINES WITH
- [SDR HNAA2012111201041](https://openairdocs.org/sdr/HNAA2012111201041.md): Warning Light · false activation · Nov 12, 2012 · N907HA · Dhav DHC8102 · Windshield/Door Rain/Ice Removal
  > RIGHT WINDSHIELD HOT LIGHT ILLUMINATED. INSPECTED SENSOR WIRING ARRANGEMENT. FOUND TO BE ON PRIMARY SENSOR. CHECKED SENSORS RESISTANCE. FOUND TO BE WITHIN LIMITS IN REF TO PPO CMM 56-10-01. SENSOR REF 30-41-00. OPS CHECKED GOOD AT THIS TIME.
- [SDR HNAA201210100110](https://openairdocs.org/sdr/HNAA201210100110.md): Door · out of rig · Oct 10, 2012 · N907HA · Dhav DHC8102 · Landing Gear Door Retract Section
  > LEFT DOOR AMBER LIGHT REMAINED ILLUMINATED WITH GEAR UP. RECYCLED GEAR STILL ILLUMINATED. FORWARD DOOR REMAINED OPEN. ACFT RETURNED TO FIELD. RERIGGED NR 1 FORWARD GEAR DOOR IAW MM32-10-21. OPS CHECKED GOOD.
- [SDR HNAA2012100901009](https://openairdocs.org/sdr/HNAA2012100901009.md): Battery · failed · Oct 9, 2012 · N907HA · Dhav DHC8102 · Emergency Lighting
  > LEFT FORWARD EXTERIOR EMERGENCY LIGHT IS DIM. R & R BATTERY. OPS CHECKED GOOD.
- [SDR HNAA2012100901005](https://openairdocs.org/sdr/HNAA2012100901005.md): Connector · damaged · Oct 9, 2012 · N907HA · Dhav DHC8102 · Light System Wiring
  > FORWARD CENTER CEILING EMERGENCY EXIT SIGN IS INOP. FOUND FORWARD CENTER CEILING LIGHT WIRE UNPLUGGED AND MATRIX CONNECTOR DAMAGED. R & R MATRIX CONNECTOR AND PLUGGED WIRES ACCORDINGLY. OPS CHECKED GOOD.
- [SDR HNAA2012100300995](https://openairdocs.org/sdr/HNAA2012100300995.md): Bolt · corroded · Oct 3, 2012 · N907HA · Dhav DHC8102 · Wing Main, Frame Structure
  > RT WING TO FUSELAGE STRUT HAD RUSTED BOLT AND BORE INSIDE OF PANEL 264CR. CLEANED BORE WITH BARREL BRUSH. CORROSION WAS TRANSFERED FROM CORRODED BOLT. INSTALLED NEW BOLT AND PLI WASHER.
- [SDR HNAA2012100300994](https://openairdocs.org/sdr/HNAA2012100300994.md): Bolt · corroded · Oct 3, 2012 · N907HA · Dhav DHC8102 · Wing Main, Frame Structure
  > AFT OTBD BOLT AND BORE IF LT AFT WING TO FUSELAGE STRUT IS RUSTED INSIDE OF PANEL 263CL. REAMED HOLE IAW DWG 85320339. CLEANED CORRSION, R & R BOLT AND PLI WASHER.
- [SDR HNAA2012100300993](https://openairdocs.org/sdr/HNAA2012100300993.md): Bolt · corroded · Oct 3, 2012 · N907HA · Dhav DHC8102 · Wing Main, Frame Structure
  > FORWARD INBD BOLT IS PITTED ON AFT STRUT, LT WING TO FUSELAGE ATTACH POINT. R & R BOLT AND PLI WASHERS.
- [SDR HNAA2012100300997](https://openairdocs.org/sdr/HNAA2012100300997.md): Floorbeam · corroded · Oct 3, 2012 · N907HA · Dhav DHC8102 · Fuselage Main, Floor Beam
  > UPPER BAG BAY FLOORBEAM ABOVE STR 31S AT BS 600 HAS CORROSION. REMOVED CORROSION FROM UPPER BAGBAY FLOORBEAM. ALODINED AND PRIMED AREA.
- [SDR HNAA2012100300996](https://openairdocs.org/sdr/HNAA2012100300996.md): Bracket · corroded · Oct 3, 2012 · N907HA · Dhav DHC8102 · Fuselage Miscellaneous Structure
  > SURFACE CORROSION AT ANGLE BRACKET JUST BELOW FLOOR AT STA X600 FRONT OF UPPER BAG BAY FLOOR. CORROSION WAS REMOVED, APPLIED ALODINE AND PRIMER TO ANGLE BRACKET AT STA X600.
- [SDR HNAA2012100100991](https://openairdocs.org/sdr/HNAA2012100100991.md): Bolt · rusted · Oct 1, 2012 · N907HA · Dhav DHC8102 · Wing, Attach Fittings
  > LEFT AFT STEEL STRUT TO WING RIB BOLT IS RUSTED AND BORE OF STRUT. REAMED HOLE TO.541 IAW DWG 85320229. CLEANED CORROSION AND R & R BOLT AND NEW PLI WASHERS.
- [SDR HNAA2012100100990](https://openairdocs.org/sdr/HNAA2012100100990.md): Seat Track · corroded · Oct 1, 2012 · N907HA · Dhav DHC8102 · Fuselage, Seat/Cargo Attach Fittings
  > MINOR CORROSION AT RIGHT OTBD SEAT TRACK AT BS 424. SEAT TRACK OUT OF LIMITS IAW RD8-53-1342. REMOVED & INSTALLED NEW SEAT TRACK IAW DWG 85320777.
- [SDR HNAA2012092800986](https://openairdocs.org/sdr/HNAA2012092800986.md): Seat Track · corroded · Sep 28, 2012 · N907HA · Dhav DHC8102 · Fuselage, Seat/Cargo Attach Fittings
  > SURFACE CORROSION AT LT OTBD SEAT TRACK AT BS 501. REMOVED CORROSION ON LT SEAT TRACK IAW RD8-53-1342. COMPLIED WITH HFEC INSPECTION. NO DEFECTS NOTED.
- [SDR HNAA2012092800985](https://openairdocs.org/sdr/HNAA2012092800985.md): Seat Track · corroded · Sep 28, 2012 · N907HA · Dhav DHC8102 · Fuselage, Seat/Cargo Attach Fittings
  > SURFACE CORROSION AT LT OTBD SEAT TRACK BS 387 THRU 366. SEAT TRACK DAMAGE IS OUT OF LIMITS. R & R SEAT TRACK IAW DWG 85320777.
- [SDR HNAA2012092800984](https://openairdocs.org/sdr/HNAA2012092800984.md): Threshold · corroded · Sep 28, 2012 · N907HA · Dhav DHC8102 · Fuselage Miscellaneous Structure
  > AIRSTAIR DOOR OPENING THRESHOLD HAS SURFACE CORROSION AROUND NUT PLACES ON TOP AND BOTTOM SIDES OF THRESHOLD. REMOVED AIRSTAIR DOOR OPENING THRESHOLD AND INSTALLED IAW DWG 85321241.
- [SDR HNAA2012092800983](https://openairdocs.org/sdr/HNAA2012092800983.md): Shear Tie · corroded · Sep 28, 2012 · N907HA · Dhav DHC8102 · Fuselage Internal Mounting Structure
  > CORROSION ON FRAME LEG AT STA X270.500 BETWEEN STR 32P AND 31P. CLEANED CORROSION, APPLIED ALODINE AND PRIMER.
- [SDR HNAA2012092800982](https://openairdocs.org/sdr/HNAA2012092800982.md): Seat Track · corroded · Sep 28, 2012 · N907HA · Dhav DHC8102 · Fuselage, Seat/Cargo Attach Fittings
  > SURFACE CORROSION AT LT INBD SEAT TRACK AT BS 330. BLENDED AFFECTED AREA TO WITHIN LIMITS OF RD8-53-1339. HFEC INSPECTION COMPLIED WITH. NO DEFECTS NOTED.
- [SDR HNAA2012092800981](https://openairdocs.org/sdr/HNAA2012092800981.md): Floorbeam · corroded · Sep 28, 2012 · N907HA · Dhav DHC8102 · Fuselage, Seat/Cargo Attach Fittings
  > SURFACE CORROSION AT BS 467 FLOORBEAM JUST BELOW LT AND RT INBD SEAT TRACK. CLEANED CORROSION. APPLIED ALODINE AND PRIMER.
- [SDR HNAA2012092600976](https://openairdocs.org/sdr/HNAA2012092600976.md): Shear Tie · corroded · Sep 26, 2012 · N907HA · Dhav DHC8102 · Fuselage Internal Mounting Structure
  > FRAME LEG AT STATION X222 HAS SURFACE CORROSION BETWEEN STR 28S AND 29S. REMOVED CORROSION AT FRAME LEG STA X222 BETWEEN STR 28S AND 29S. APPLIED ALODINE AND PRIMER TO AREA.
- [SDR HNAA2012092600975](https://openairdocs.org/sdr/HNAA2012092600975.md): Frame · corroded · Sep 26, 2012 · N907HA · Dhav DHC8102 · Fuselage Main, Frame
  > STRINGER 31S AND FRAME LEG IS CORRODED AT STATION X222. CLEANED CORROSION FROM FRAME LEG AND STRINGER 31S AT STA X222. APPLIED ALODINE AND PRIMED AREA.
- [SDR HNAA2012092600974](https://openairdocs.org/sdr/HNAA2012092600974.md): Shear Tie · corroded · Sep 26, 2012 · N907HA · Dhav DHC8102 · Fuselage Internal Mounting Structure
  > CORROSION AT FRAME LEG X240.500 BETWEEN STR. 28P AND 27P. REMOVED BRACKET FROM FRAME AT STA.X240.500. REMOVED FRAME SECTION AT STA X240.500, FORMED AND HEAT TREATED FRAME MEMBER IAW DWG 85320497. ALODINED AND PRIMED AS REQUIRED. COMPLIED WITH CONDUCTIVITY T
- [SDR HNAA2012092600973](https://openairdocs.org/sdr/HNAA2012092600973.md): Stringer · corroded · Sep 26, 2012 · N907HA · Dhav DHC8102 · Fuselage Main, Longeron/Stringer
  > CORROSION AT STRINGER 28P WHERE IT MEETS MAIN FRAME X387.350. REMOVED BRACKET ON STRINGER 28P ATTACH POINT TO MAIN FRAME X387.350. CLEANED MINOR SURFACE CORROSION FROM STRINGER AND APPLIED ALODINE AND PRIMER.
- [SDR HNAA2012092600972](https://openairdocs.org/sdr/HNAA2012092600972.md): Shear Tie · corroded · Sep 26, 2012 · N907HA · Dhav DHC8102 · Fuselage Internal Mounting Structure
  > FRAME LEG AT STATION X242 BETWEEN STR 31S AND 30S HAS SURFACE CORROSION. REMOVED CORROSION FROM FRAME LEG AT STA X242 BETWEEN STR 31S AND 30S. APPLIED ALODINE AND PRIMER.
- [SDR HNAA2012092600971](https://openairdocs.org/sdr/HNAA2012092600971.md): Stringer · corroded · Sep 26, 2012 · N907HA · Dhav DHC8102 · Fuselage Main, Longeron/Stringer
  > STRINGER 31S HAS CORROSION BETWEEN FRAME X242 AND X201. REPAIRED IAW RD8-53-3044. PERFORMED HFEC INSPECTION. NO DEFECTS NOTED. APPLIED ALODINE AND EPOXY PRIMER IAW RD8-53-3044.
- [SDR HNAA2012092600970](https://openairdocs.org/sdr/HNAA2012092600970.md): Floor Support · corroded · Sep 26, 2012 · N907HA · Dhav DHC8102 · Fuselage Miscellaneous Structure
  > SEVERAL AREAS OF LIGHT CORROSION ON OTBD FLOOR SUPPORT, AROUND AFT ATTACH HOLE FOR WARDROBE FLOOR. CLEANED CORROSION FROM OTBD FLOOR SUPPORT. ALODINED AND PRIMED AREA AS REQUIRED.
- [SDR HNAA2012092600969](https://openairdocs.org/sdr/HNAA2012092600969.md): Door · corroded · Sep 26, 2012 · N907HA · Dhav DHC8102 · Fluid Service Doors
  > LAVATORY SERVICE DOOR IS CORRODED. REMOVED CORRODED LAVATORY DOOR. INSTALLED NEW LAVATORY DOOR ASSY IAW DWG 85320983.
- [SDR HNAA2012092600968](https://openairdocs.org/sdr/HNAA2012092600968.md): Doubler · corroded · Sep 26, 2012 · N907HA · Dhav DHC8102 · Fuselage Main, Plate/Skin
  > LAVATORY MACHINED DOUBLER ON CUTOUT IS CORRDED. REMOVED MACHINE DOUBLER, INSTALLED NEW MACHINED DOUBLER IAW DWG 85320983.
- [SDR HNAA2012092500967](https://openairdocs.org/sdr/HNAA2012092500967.md): Frame · corroded · Sep 25, 2012 · N907HA · Dhav DHC8102 · Fuselage Main, Frame
  > CORROSION AT FRAME STA X434.500 AND STR 22P. REMOVED 1 AFT ANGLE AT MAIN FRAME, STRINGER TO SEAT RAIL WEB AND ANGLE FROM STA 443, STRINGER TIE. CLEANED, BLENDED LIGHT CORROSION TO WITHIN LIMITS. ALODINE AND PRIMED. REINSTALLED IAW SRM 51-20-11 AND DWG 8533
- [SDR HNAA2012092500966](https://openairdocs.org/sdr/HNAA2012092500966.md): Frame · corroded · Sep 25, 2012 · N907HA · Dhav DHC8102 · Fuselage Main, Frame
  > CORROSION AT FRAME BS 445.500 AND STR. 22P. REMOVED CLEAT AND BLENDED TO WITHIN LIMITS IAW SRM 51-20-11. ALODINE AND PRIMED. REINSTALLED IAW DWG 85320511.
- [SDR HNAA2012092500965](https://openairdocs.org/sdr/HNAA2012092500965.md): Frame · corroded · Sep 25, 2012 · N907HA · Dhav DHC8102 · Fuselage Main, Frame
  > CORROSION AT "L" BRACKET ON BOTH SIDES OF MAIN FRAME STA X383, STR 22P. REMOVED FORWARD AND AFT ANGLE ON MAIN FRAME AT STA.X387. BLENDED LIGHT CORROSION TO WITHIN LIMITS IAW SRM 51-20-11. ALODINED, PRIMED AND REINSTALLED IAW DWG 85320777.

Next page: https://openairdocs.org/deregistered/N907HA-2016-09-20/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 = 'N907HA' AND deregistration_id = 'N907HA-2016-09-20'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N907HA-2016-09-20/reports

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