# Service difficulty reports: N505DA, cancelled Mar 21, 2013

A list on [N505DA, cancelled Mar 21, 2013](https://openairdocs.org/deregistered/N505DA-2013-03-21.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 2 · 66 reports

- [SDR DL72L011283](https://openairdocs.org/sdr/DL72L011283.md): Light · inoperative · Aug 3, 2001 · N505DA · Boeing 727232 · Passenger Compartment Lighting
  > ON LAYOVER FOUND 4CD FASTEN SEAT BELT LIGHT INOP. C/A RELAMPED OPS CKS GOOD
- [SDR DL72L011149](https://openairdocs.org/sdr/DL72L011149.md): Switch · out of adj · Jul 11, 2001 · N505DA · Boeing 727232 · Leading Edge Slat Control System
  > AT 5 DEG FLAPS NR 3 L/E FLAP DID NOT EXTEND FULLY CYCLED. ACCORDING TO CHECKLIST BUT DID NOT EXTEND. ADJUSTED NR 3 L/E FLAP SWT RAN FLAPS TO 5 DEG AND BACK ALL IND NORMAL.
- [SDR DL72L010335](https://openairdocs.org/sdr/DL72L010335.md): Battery · discharged · Feb 27, 2001 · N505DA · Boeing 727232 · Emergency Lighting
  > ON L/O, FOUND 1L OVERHEAD EMERGENCY EXIT SIGN DIM. REPLACED EXIT SIGN BATTERIES, CKS OK.
- [SDR DL72L010309](https://openairdocs.org/sdr/DL72L010309.md): Web · cracked · Feb 21, 2001 · N505DA · Boeing 727232 · Fuselage Main, Structure
  > A 1 INCH CRACK IN LT TORQUE BOX VERT WEB AT UPPER RIVET ROW STA 1210 AND TWO CRACKS IN LT TORQUE BOX VERT WEB AT UPPER RIVET ROW STA 1235. REPAIR PER M/M 53-11-000-8.
- [SDR DL72L001381](https://openairdocs.org/sdr/DL72L001381.md): Angle · cracked · Jul 21, 2000 · N505DA · Boeing 727232 · Fuselage Miscellaneous Structure
  > FOUND ON B1 LETTER CK, 1.5 INCH CRACK IN STA 870 WEB VERTICAL CHORD AT I/B END OF LT WHEEL WELL. REPAIRED PER B727 DRD 53-10-9D FIG 806.
- [SDR DL72L000352](https://openairdocs.org/sdr/DL72L000352.md): Actuator · leaking · Feb 21, 2000 · N505DA · Boeing 727232 · Drag Control Actuator
  > LOST B HYDRAULIC SYSTEM PRESS AND FLUID IN FLIGHT. MADE UNSCHEDULED LANDING. FOUND NUMBER 3 SPOILER ACTUATOR LEAKING. REPLACED NR 3 SPOILER ACTUATOR.
- [SDR DL72L992760](https://openairdocs.org/sdr/DL72L992760.md): Web · dent · Dec 16, 1999 · N505DA · Boeing 727232 · Vertical Stabilizer
  > THE NR 4 RIB OF THE VERTICAL STABILIZER HAS A DENT IN THE WEB THAT RESULTED IN A 1 INCH DIAMETER CUTOUT. THE DAMAGE WAS FOUND AT HMV AND REPAIRED PER ERA 333924-14.
- [SDR DL72L992782](https://openairdocs.org/sdr/DL72L992782.md): Rib · cracked · Dec 1, 1999 · N505DA · Boeing 727232 · Leading Edge Devices
  > AT HMV2 FOUND NR 3 SLAT RIBS CRACKED. REPAIR AT RIB MARKED NR 3, RIB MKD NR 10, RIB MKD NR 17. CORROSION - DYE CKD AS PER PS 900-6-3 AND NO CRACKS. FABRICATED DOUBLER PER MM 57-54-0 PG 807. INSTALLED DOUBLER PER SAME, DYE CHECKED RIB NR 17 PER PS 900-6-3
- [SDR DL72L992727](https://openairdocs.org/sdr/DL72L992727.md): Rib · crack · Dec 1, 1999 · N505DA · Boeing 727232 · Leading Edge Devices
  > AT HMV2, FOUND NR 4 SLAT RIB (MARKED) CRACKED. FABRICATED DOUBLER PER MM 57-54-0 FIG 804. DYE CHECKED END OF CRACK PER FIG 504. CHEM TESTED PER PS 900-2-4-1 NR 2. REPAIRED RIB PER MM 57-54-0.
- [SDR DL72L992671](https://openairdocs.org/sdr/DL72L992671.md): Rib · cracked · Dec 1, 1999 · N505DA · Boeing 727232 · Leading Edge Devices
  > AT HMV2, FOUND NR 8 SLAT RIB'S CRACKED, NR 4, 14 (MARKED). REMOVED I/B SLTRK AND STOP DRILLED CRACK PER MM 57-40-0 FIG 809, FABRICATED REPAIR PARTS PER MM 57-54-00 FIG 809.
- [SDR DL72L992783](https://openairdocs.org/sdr/DL72L992783.md): Skin · torn · Nov 30, 1999 · N505DA · Boeing 727232 · Elevator, Plate/Skin
  > AT HMV2 ELEVATOR T/E CHIPPED/TORN LT ELEVATOR EXTREME O/B END. BUSHED AREA AND FOUND TO BE WITHIN LIMITS PER SRM 55-20-1 FIG 161, INSTALLED FASTENERS.
- [SDR DL72L992670](https://openairdocs.org/sdr/DL72L992670.md): Skin · disbonded · Nov 30, 1999 · N505DA · Boeing 727232 · Elevator, Plate/Skin
  > AT HMV2, FOUND RT ELEV T/E DISBONDED BETWEEN UPPER AND LWR SKIN SEVERAL AREA'S FROM I/B TO O/B AREA. REPAIRED PER MM 55-20-0 PG 801 NR 2.
- [SDR DL72L992669](https://openairdocs.org/sdr/DL72L992669.md): Skin · delaminated · Nov 30, 1999 · N505DA · Boeing 727232 · Elevator, Plate/Skin
  > AT HMV2, FOUND LT ELEVATOR T/E DELAMINATED I/B AND O/B OF TAB. REPAIRED PER MM 55-20-0 PG 801 NR 2.
- [SDR DL72L992668](https://openairdocs.org/sdr/DL72L992668.md): Skin · disbonded · Nov 30, 1999 · N505DA · Boeing 727232 · Elevator, Plate/Skin
  > AT HMV2, FOUND RT ELEVATOR I/B TRAILING EDGE DISBONDED. REPAIRED PER MM 55-20-0 PG 801 NR 2.
- [SDR DL72L992667](https://openairdocs.org/sdr/DL72L992667.md): Stringer · cracked · Nov 30, 1999 · N505DA · Boeing 727232 · Vertical Stabilizer, Spar/Rib
  > AT HMV2, FOUND STRINGER 5R CRACKED AT RIB NR 9 VERT STAB INTERIOR. DYE CHECKED AND FOUND CRACK EXTENDS TO EDGE OF MATERIAL. CHEM TREATED PER PS 900-2-4-1 NR 2, FABRICATED REPAIR PER MM 55-30-0 PG 803, AND INSTALLED PER SAME.
- [SDR DL72L992254](https://openairdocs.org/sdr/DL72L992254.md): Socket · failed · Oct 10, 1999 · N505DA · Boeing 727232 · Emergency Lighting
  > PILOT REPORT, FIRST CLASS SECTION EMERGENCY TRACK LIGHTING INOP. FOUND BAD SOCKET AT 10DEF REPLACED FUSE AT FWD POWER SUPPLY PACK. SYSTEM OPS NORMAL DEFERED SOCKET AT 10DEF PER MEL 33-00-17B SOCKET DISCONECTED AND WIRE HARNESS SECURED. REPLACED SEAT MOUNTED
- [SDR DL72L991809](https://openairdocs.org/sdr/DL72L991809.md): Frame · cracked · Aug 11, 1999 · N505DA · Boeing 727232 · Fuselage Miscellaneous Structure
  > FUSELAGE C1 DOOR SURROUND FRAME, FS 560, WEB CRACK REPAIR. A INCH 2 CRACK WAS FOUND IN THE WEB OF THE FORWARD JAMB FRAME OF THE C1 DOOR OPENING. THE CRACK WAS LOCATED AT THE 2ND FROM THE TOP DOOR STOP. THE CRACK WAS ROUTED OUT AND REPAIRED WITH A DOUBLER
- [SDR DL72L991795](https://openairdocs.org/sdr/DL72L991795.md): Web · cracked · Aug 11, 1999 · N505DA · Boeing 727232 · Fuselage Miscellaneous Structure
  > 1 INCH CRACK AT RIGHT TORQUE BOX VERTICAL WEB AT UPPER RIVET ROW STA 1223 (48 SEC). REPAIR PER MM 53-11-0.
- [SDR DL72L991459](https://openairdocs.org/sdr/DL72L991459.md): Accessory Unit · inoperative · Jun 28, 1999 · N505DA · Boeing 727232 · Landing Gear Position and Warning
  > GEAR EXTENSION BUF UNSAFE GEAR WARNING WITH RT MAIN GEAR RED INDICATOR LIGHT ON WITHOUT THE GREEN DOWN AND SAFE LIGHT ON. REPLACED LANDING GEAR ACCESSORY UNIT.
- [SDR DL72L991225](https://openairdocs.org/sdr/DL72L991225.md): Skin · cracked · May 31, 1999 · N505DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > INTERNAL HFEC INSPECTION OF THE LOWER FASTENER ROW OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 360 AND 480 INDICATED 2 CRACKS BETWEEN FS 440 AND 460. THE CRACKS WERE CUT OUT OF THE SKIN LAP AND REPAIRED WITH AN ALUMINUM DOUBLER PER B727 SRM 53-30-3, FIG 5
- [SDR DL72L991224](https://openairdocs.org/sdr/DL72L991224.md): Skin · cracked · May 31, 1999 · N505DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > INTERNAL HFEC INSPECTION OF THE LOWER FASTENER ROW OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 680 AND 740 INDICATED 8 CRACKS ALONG THE PANEL LENGTH. THE SKIN LAP WAS CUT OUT ALONG THE PANEL LENGTH AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER ER/A 3
- [SDR DL72L991223](https://openairdocs.org/sdr/DL72L991223.md): Skin · cracked · May 31, 1999 · N505DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 481 AND 681 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED 47 CRACKS ALONG THE PANEL LENGTH. THE ENTIRE SKIN LAP WAS CUT OUT AND REPAIRED WITH AN
- [SDR DL72L990764](https://openairdocs.org/sdr/DL72L990764.md): Battery · discharged · Apr 7, 1999 · N505DA · Boeing 727232 · Emergency Lighting
  > RT OVERWING EMERGENCY LIGHT INOP. REPLACED BATTERY AT M957, OPS CHECKS GOOD.
- [SDR DL72L990318](https://openairdocs.org/sdr/DL72L990318.md): Frame · damaged · Feb 14, 1999 · N505DA · Boeing 727232 · Fuselage Main, Frame
  > FUSELAGE LT OVERWING EXIT CUTOUT FRAME FS 784, REPAIR FOR DISCREPANT FASTENER HOLES. WHILE ACCOMPLISHING INSPECTIONS OF THE LT OVERWING EXIT CUTOUT FRAME AT FS 784, SEVERAL FASTENER HOLES WERE FOUND OVERSIZED DAMAGED. THE MODIFICATION PER BAC S/B 727-53-0197
- [SDR DL72L990317](https://openairdocs.org/sdr/DL72L990317.md): Frame · damaged · Feb 14, 1999 · N505DA · Boeing 727232 · Fuselage Main, Frame
  > FUSELAGE RT OVERWING EXIT CUTOUT FRAME FS 783.95, REPAIR FOR DAMAGED HOLES. UPON INSPECTION FOR TYPICAL CRACKS IN THE INNER CHORD OF THEFS 783.95 OVERWING EXIT CUTOUT FRAME, SEVERAL HOLES WERE FOUND MISDRILLED. THE PREVENTATIVE MODIFICATION PER BAC S/B 727-5
- [SDR DL72L990316](https://openairdocs.org/sdr/DL72L990316.md): Frame · cracked · Feb 14, 1999 · N505DA · Boeing 727232 · Fuselage Main, Frame
  > FUSELAGE RT OVERWING EXIT FRAME, FS 761, FRAME CHORD REPAIR. THE FS 761 FRAME FOR THE RT OVERWING EXIT CUTOUT WAS FOUND WITH A TYPICAL CRACK IN THE INNER CHORD. THE FRAME WAS REPAIRED/MODIFIED PER BAC S/B 727-53-0197 WITH MODIFICATIONS REQUIRED DUE TO EX
- [SDR DL72L990275](https://openairdocs.org/sdr/DL72L990275.md): Support · corroded · Feb 10, 1999 · N505DA · Boeing 727232 · Wing Miscellaneous Structure
  > WING MLG SUPPORT BEAM, LT AFT ATTACH LUG, REPAIR FOR CORRODED LUG. THE AFT ATTACH LUG OF THE LT MLG SUPPORT BEAM WAS FOUND CORRODED. THE CORROSION WAS REMOVED BY OVERSIZING THE LUG HOLE BORE AND SPOTFACING THE SURFACE OF THE LUG. THE LUG WAS REPAIRED BY INS
- [SDR DL72L990184](https://openairdocs.org/sdr/DL72L990184.md): Skin · gouged · Jan 26, 1999 · N505DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > A GOUGE WAS FOUND IN THE SKIN PANEL AT FS 500 BELOW THE STRINGER 26L LAP SPLICE. THE DAMAGE WAS TRIMMED OUT OF THE SKIN WITHOUT DAMAGING THE EXISTING LAP. THE CUTOUT WAS REPAIRED PER B727 SRM 53-30-3, FIG 5 AND DOCUMENTED PER ER/A 366548-14.
- [SDR DL72L990039](https://openairdocs.org/sdr/DL72L990039.md): Skin · cracked · Jan 7, 1999 · N505DA · Boeing 727232 · Leading Edge Devices
  > NR 7 SLAT LOWER COVE SKIN ATTACH ANGLE CRACKED AT I/B STOP PAD. REPAIRED PER MM 57-54-0.
- [SDR DL72L982657](https://openairdocs.org/sdr/DL72L982657.md): Line · cracked · Dec 30, 1998 · N505DA · Boeing 727232 · Hydraulic System, Main
  > CREW LOST B HYDRAULICS PRESSURE AND QUANTITY ON ARRIVAL TO PHL. FOUND BROKEN HYDRAULIC LINE IN HYD SERVICE BAY REF IPC-29- 14-00-06 ITEM 160. MPN-65-17849-61M. DPN-294201161. INSTALLED TEMP HYDRAULIC LINE, SERVICED HYD SYS TO FULL AND LEAK CHKS NORMAL. FWD
- [SDR DL72L982470](https://openairdocs.org/sdr/DL72L982470.md): Stop · loose · Nov 27, 1998 · N505DA · Boeing 727232 · Leading Edge Devices
  > WING NR 7 SLAT, DOWNSTOP FITTING, REPAIR FOR LOOSE BOLT. THE NR 7 SLAT DOWNSTOP FITTINGS WERE FOUND WITH LOOSE BOLTS. DURING INSPECTIONS PER S/B 727-57-171. THE STOP FITTINGS FOR THE SLAT WERE MODIFIED PER THE REQUIREMENTS OF THE S/B. THE MODIFICATION OF
- [SDR DL72L982374](https://openairdocs.org/sdr/DL72L982374.md): Battery Pack · discharged · Nov 16, 1998 · N505DA · Boeing 727232 · Emergency Lighting
  > RIGHT AFT EMERGECY OVERWING LIGHTS ON AFT CARGO DOOR INOP. REPLACED BATTERY PACK.
- [SDR DL72L981187](https://openairdocs.org/sdr/DL72L981187.md): Mount · cracked · Jun 3, 1998 · N505DA · Boeing 727232 · Leading Edge Slat Actuator
  > NR 1 LE FLAP ACTUATOR MOUNT CRACKED UPPER O/B CORNER. REPAIR PER M/M 57-20-21.
- [SDR DL72L981186](https://openairdocs.org/sdr/DL72L981186.md): Skin · delaminated · Jun 3, 1998 · N505DA · Boeing 727232 · Elevator, Plate/Skin
  > 5 IN LENGTH DELAMINATION ON RT ELEVATOR TRAILING EDGE I/B END. REPAIR PER M/M 55-20-0.
- [SDR DL72L981185](https://openairdocs.org/sdr/DL72L981185.md): Web · cracked · Jun 3, 1998 · N505DA · Boeing 727232 · Fuselage Miscellaneous Structure
  > .1875 IN CRACK ON VERTICAL WEB LIGHTNING HOLE STA 1228 LT SIDE. ROUTE CRACK PER M/M 53-11-0.
- [SDR DL72L981184](https://openairdocs.org/sdr/DL72L981184.md): Casting · cracked · Jun 3, 1998 · N505DA · Boeing 727232 · Drag Control Actuator
  > 0/B ACTUATOR ATTACH CASTING BROKEN AT LOWER MOUNT BOLT NR 4 SPOILER. REPLACED CASTING PER M/M 57-42-0.
- [SDR DL72L980646](https://openairdocs.org/sdr/DL72L980646.md): Air Distribution · smoke · Mar 24, 1998 · N505DA · Boeing 727232 · Air Distribution System
  > AIR RETURN SMOKE IN AFT CABIN DURNING T/O CREW DUMPED FUEL TO 163,500 NORMAL LANDING AND STOP. RAN PACKS WITH APU AIR ALL PACKS OPERATED NORMAL. FLT CREW TAXI AND AND RAN ENGINES AT RUNUP AREA WITH MECHANIC, CHECKING PACKS WITH ENGINE AIR AT IDLE AND POWER.
- [SDR DL72L980266](https://openairdocs.org/sdr/DL72L980266.md): Light · inoperative · Jan 30, 1998 · N505DA · Boeing 727232 · Emergency Lighting
  > L-2 DOOR OVERHEAD EMERGENCY LIGHT INOP. REPLACED LIGHT ASSY, CKS GOOD.
- [SDR DL72L972116](https://openairdocs.org/sdr/DL72L972116.md): Spar · cracked · Oct 13, 1997 · N505DA · Boeing 727232 · Elevator, Spar/Rib
  > THE REAR SPAR OF THE RT ELEVATOR IS CRACKED ON THE LOWER I/B SIDE OF THE SECOND FROM THE I/B HINGE FITTING. THE CRACK IS APPROXIMATELY.25 LONG. THIS CRACK LENGTH IS WITHIN THE.250 STOP DRILL LIMITS OF BAC S/B 727-55-0089. THE CRACK WILL BE STOP-DRILLED UN
- [SDR DL72L971429](https://openairdocs.org/sdr/DL72L971429.md): Battery Pack · discharged · Jul 21, 1997 · N505DA · Boeing 727232 · Emergency Lighting
  > AFT FLOOR EMERGENCY LIGHTS INOP. REPLACED BATTERY RACK M9027, ALL OPS NORMAL.
- [SDR DL72L970933](https://openairdocs.org/sdr/DL72L970933.md): Rear Spar · cracked · May 14, 1997 · N505DA · Boeing 727232 · Elevator, Spar/Rib
  > THE REAR SPAR OF THE RT ELEVATOR IS CRACKED ON THE LOWER INBD SIDE OF THE SECOND FROM INBD HINGE FITTING. THE CRACK IS APPROX.25 INCH LONG. THIS CRACK LENGTH IS WITHIN THE 0.250 STOP DRILL LIMITS OF BAC S/B 727-55-0089. THE CRACK WILL BE STOP-DRILLED (TEMP
- [SDR DL72L961135](https://openairdocs.org/sdr/DL72L961135.md): Light · frayed wires · May 12, 1996 · N505DA · Boeing 727232 · Emergency Lighting
  > EMERGENCY LIGHTS OUT FROM ROWS 12 TO 19. FOUND FRAYED WIRES RUBBING AT ROW 17. REPLACED BULB SOCKET, FUSES IN M9026 AND M9027 POWER SUPPLIES, OP CKS NORMAL.
- [SDR DL72L960878](https://openairdocs.org/sdr/DL72L960878.md): Light · inoperative · Apr 16, 1996 · N505DA · Boeing 727232 · Emergency Lighting
  > FWD ENTRY OVERHEAD EMERGENCY LIGHT INOP. REPLACED LIGHT ASSY, CKS GOOD.
- [SDR DL72L960833](https://openairdocs.org/sdr/DL72L960833.md): Slide · torn webbing · Mar 31, 1996 · N505DA · Boeing 727232 · Escape Slide
  > ON PREFLIGHT, FOUND RT AFT SERVICE DOOR EMERGENCY SLIDE WEBBING AT GIRT BAR TORN. REPLACED SLIDE.
- [SDR DL72L960622](https://openairdocs.org/sdr/DL72L960622.md): Compressor · stalled · Mar 20, 1996 · N505DA · Boeing 727232 · Turbine Engine Compressor Section
  > APPLYING TAKEOFF POWER HAD EXPERIENCED COMPRESSOR STALLS ON NR 2 ENG, WIND WAS APPROX 320 AT 17 TO 20 KTS, DEPARTED 35L DFW. AFTER TAKEOFF COMPRESSOR STALLS RETURNED ON CLIMBOUT AT 190 KTS. REPLACED PRBC AND P AND D VLV, NO HELP. ACTVATED 6TH STAGE BLEED P
- [SDR DL72L960614](https://openairdocs.org/sdr/DL72L960614.md): Power Supply · inoperative · Mar 19, 1996 · N505DA · Boeing 727232 · Emergency Lighting
  > DURING EMERGENCY LIGHTING CHECK, MAINT FOUND TRACK LIGHTING BETWEEN ROWS 12 AND 19 INOP. REPLACED POWER SUPPLY, OPERATION NORMAL.
- [SDR DL72L960500](https://openairdocs.org/sdr/DL72L960500.md): Angle · cracked · Mar 5, 1996 · N505DA · Boeing 727232 · Leading Edge Devices
  > FOUND ON D1 LETTER CK, NR 7 SLAT LOWER ANGLE CRACKED AT THE ANTI-ICE DUCT CUTOUT. REPAIRED PER MM 57-54-0.
- [SDR DL72L960499](https://openairdocs.org/sdr/DL72L960499.md): Angle · cracked · Mar 5, 1996 · N505DA · Boeing 727232 · Leading Edge Slat Actuator
  > FOUND ON D1 LETTER CK, NR 6 L/E FLAP ACTUATOR SUPPORT BOX CRACKED INBD END. REPAIRED PER MM 57-20-21.
- [SDR DL72L960498](https://openairdocs.org/sdr/DL72L960498.md): Casting · cracked · Mar 5, 1996 · N505DA · Boeing 727232 · Leading Edge Slat Actuator
  > FOUND ON D1 LETTER CK, NR 2 SLAT ACTUATOR MOUNT CASTING/ANGLE CRACKED O/B UPPER EAR. REPAIRED PER MM 57-42-0.
- [SDR DL72L954319](https://openairdocs.org/sdr/DL72L954319.md): Eel Charger · malfunctioned · Oct 29, 1995 · N505DA · Boeing 727232 · Emergency Lighting
  > ON PREFLIGHT, EMERGENCY EXIT LIGHTING BATTERY CHARGER POPS CIRCUIT BREAKER. T/S SYS REPLACED BATT CHARGER C/B AND SPLICE SM17 WDM 33-51-02 PG 5, OPERATION NORMAL.

Next page: https://openairdocs.org/deregistered/N505DA-2013-03-21/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 = 'N505DA' AND deregistration_id = 'N505DA-2013-03-21'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N505DA-2013-03-21/reports

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