# Service difficulty reports: N246FE, cancelled Jul 28, 2009

A list on [N246FE, cancelled Jul 28, 2009](https://openairdocs.org/deregistered/N246FE-2009-07-28.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 · 57 reports

- [SDR 08FDEA04015](https://openairdocs.org/sdr/08FDEA04015.md): Transmitter · malfunctioned · Sep 24, 2008 · N246FE · Boeing 727277 · Engine Pressure Ratio (EPR)
  > WITH T/O PWR SET ENGINE NR 3 N1 WAS 87 PECENT WITH EPR SET AT STD PWR 2.12, DEFERED EPR INDICATION. REMOVED AND REPLACED THE EPR TRANSMITTER.
- [SDR 08FDEA00089](https://openairdocs.org/sdr/08FDEA00089.md): Frame · cracked · Jan 10, 2008 · N246FE · Boeing 727277 · Fuselage Main, Frame
  > LOWER FWD CARGO, SPLICE FRAME AT ST 580, STR 22L IS CRACKED. VERIFIED BY HFEC. REMOVED 53FX1350 SPLICE FRAME, FABRICATED AND INSTALLED NEW SPLICE FRAME IAW FEDEX DRWG 53FX1350 REV A AND 727-200 SRM 51-30-2.
- [SDR 07FDEA02786](https://openairdocs.org/sdr/07FDEA02786.md): Smoke Detector · failed · Aug 7, 2007 · N246FE · Boeing 727277 · Smoke Detection
  > DESCENT BELL SOUNDED MAIN FIRE LIGHT ILLUMINATED, SMOKE ILLUMINATED. EMERGENCY DECLARED. FUMES WERE PRESENT IN THE COCKPIT. ALL EMERGENCY QRH CHECKLIST ACCOMPLISHED. WHILE ENTERING A/C NOTICED NO ODOR OF ANY SORT, INSPECTED A/C FOR ANY SIGNS OF HEAT STR
- [SDR 07FDEA00627](https://openairdocs.org/sdr/07FDEA00627.md): Receptacle · cracked · Dec 22, 2006 · N246FE · Boeing 727277 · Nacelle/Pylon, Main Frame
  > THREE RECEPTACLES DEFECTIVE ON NR 3 PYLON STRUCTURE WHERE PANEL 5402 MOUNTS TO PYLON. REPLACED THE DEFECTIVE RECEPTACLES AT PYLON PANEL 5502 MOUNT AREA. IAW 727-200 SRM 51-30-2. REINSTALLED PANEL 5502.
- [SDR 06FDEA04305](https://openairdocs.org/sdr/06FDEA04305.md): Beam · cracked · Dec 22, 2006 · N246FE · Boeing 727200 · Cargo/Baggage Doors
  > NR 3 CARGO DOOR, LWR BEAM CRACKED FWD END. REPAIRED IAW EA 7-5230-106835 PT1 REF WRI 52-30/8690.
- [SDR 06FDEA0984](https://openairdocs.org/sdr/06FDEA0984.md): Warning System · activated · Mar 8, 2006 · N246FE · Boeing 727200 · Leading Edge Slat Control System
  > ON TAKEOFF ROLL LED INDICATIONS WENT AMBER THEN BACK TO GREEN, AT 45-60 KTS WENT AMBER. TAKEOFF REJECTED.
- [SDR 04FDEA02573](https://openairdocs.org/sdr/04FDEA02573.md): Frame · cracked · Aug 29, 2004 · N246FE · Boeing 727200 · Fuselage Main, Frame
  > RIGHT MLG WHEEL WELL 870 BULKHEAD I/B LWR SUPPORT FRAME IS CRACKED JUST I/B OF BLEED AIR SHUTOFF VALVE.
- [SDR 04FDEA02563](https://openairdocs.org/sdr/04FDEA02563.md): Frame · cracked · Aug 25, 2004 · N246FE · Boeing 727200 · Fuselage Main, Frame
  > COMPLY WITH EO 7-5310-7-3367 PT 9 FOR CRACK IN 783.95 FRAME RT. *S/D* COMPLIED WITH EO 7-5310-7-3367 PT 9.
- [SDR 04FDEA02552](https://openairdocs.org/sdr/04FDEA02552.md): Frame · damaged · Aug 23, 2004 · N246FE · Boeing 727200 · Fuselage Main, Frame
  > FRAME DAMAGED AT BS 1166, BETWEEN STRINGER 3 AND 4 RT. *S/D* REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR DOUBLER AT BS 1166 BETWEEN STR 3 & 4 IAW SRM 51-40-3.
- [SDR 04FDEA02551](https://openairdocs.org/sdr/04FDEA02551.md): Skin · chafed · Aug 23, 2004 · N246FE · Boeing 727200 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN CHAFED STA 720D 12 STR 19L. *S/D* REPAIRED DAMAGED UPPER SKIN AT BS 720D PLUS 12 STR 19L PER SRM 53-30-3 DETAIL 2 & FED EX SR27-57-056 DRAWING.
- [SDR 04FDEA02530](https://openairdocs.org/sdr/04FDEA02530.md): Skin · bent · Aug 19, 2004 · N246FE · Boeing 727200 · Fuselage Main, Plate/Skin
  > AFT CARGO DOOR CUTOUT LOWER EDGE SKIN /DOUBLERS ARE BENT. REPAIRED DAMAGED AFT CARGO DOOR CUT-OUT SKIN/DOUBLERS PER EA 7-5330-55360
- [SDR 04FDEA02529](https://openairdocs.org/sdr/04FDEA02529.md): Doubler · damaged · Aug 19, 2004 · N246FE · Boeing 727200 · Fuselage Main, Plate/Skin
  > NR 1400, RT STA 600-620 STR 9, SKIN REPAIR DOUBLER REQUIRES FURTHER EVALUATION. REMOVED SKIN DOUBLER AT STA 600 STR 9 RH AND REPAIRED PER SRM 53-30-3 FIG 3, REPAIRED DAMAGED STRINGER AT STA 600 9 RH PER SRM 53-10-3 AND REPAIRED DAMAGED TEAR STRAP AT STA 600
- [SDR 04FDEA02500](https://openairdocs.org/sdr/04FDEA02500.md): Shear Tie · corroded · Aug 18, 2004 · N246FE · Boeing 727200 · Fuselage Main, Structure
  > CORROSION ON FWD FLANGE OF FRAME SHEAR TIE AT BS 480 BETWEEN STR 27L AND 28L. *S/D* REMOVED CORROSION ON FWD FLANGE OF FRAME SHEAR TIE STA 480 BETWEEN STR 27L AND 28L. REMOVED 021. 1 X 1 INCH FROM.063, OUT OF LIMITS. REMOVED DAMAGED AREA, FABRICATED REPAI
- [SDR 04FDEA02493](https://openairdocs.org/sdr/04FDEA02493.md): Frame · cracked · Aug 17, 2004 · N246FE · Boeing 727200 · Fuselage Main, Frame
  > CRACKED OUTER FRAME ANGLE STA 804.5 STR 14R. *S/D* REMOVED & REPLACED ANGLE AT BS 804.5 STR 14R PER SRM 51-30-2 & 51-10-1.
- [SDR 04FDEA02492](https://openairdocs.org/sdr/04FDEA02492.md): Floorbeam · corroded · Aug 17, 2004 · N246FE · Boeing 727200 · Fuselage Main, Floor Beam
  > CORROSION ON FLOORBEAM BS 312 WL 208 LBL 3-47 AT FASTENER AND NUT PLATE HOLES. REMOVED CORROSION ON FLOORBEAM STA 312, W/L 208, LBL 3-47, AT FASTENER & NUT PLATE HOLES, REMOVED 5 X 2 INCH LBL 3 FROM.090. LBL 4 4 X 2 X.0015 INCH. LBL 20 6 X 2 X.005 INCH, L
- [SDR 04FDEA02490](https://openairdocs.org/sdr/04FDEA02490.md): Frame · bent · Aug 17, 2004 · N246FE · Boeing 727200 · Fuselage Main, Frame
  > FRAME BENT BS 950F AT STR 26 LT, AFT CARGO BAY. *S/D* FRAME DENT BS 950F AT STR 26 LT AFT CARGO FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. REPAIRED FRAME PER SRM 51-40-3.
- [SDR 04FDEA02474](https://openairdocs.org/sdr/04FDEA02474.md): Floorbeam · corroded · Aug 13, 2004 · N246FE · Boeing 727200 · Fuselage Main, Floor Beam
  > CORROSION IN COCKPIT AT 25G BEAM UPPER FLANGE BS 267 WL 208. REMOVED AND REPLACED G-BEAM CHORD IAW SRM 51-30-5, 51-30-2, 51-30-8.
- [SDR 04FDEA02473](https://openairdocs.org/sdr/04FDEA02473.md): Frame · dented · Aug 13, 2004 · N246FE · Boeing 727200 · Fuselage Main, Frame
  > FWD CARGO COMPARTMENT FRAME DENTED STA 680 ABOVE STR 24L. REPAIRED BS 680. FRAME AT STR 24L IAW SRM 51-40-3 FIG 1.
- [SDR 04FDEA02472](https://openairdocs.org/sdr/04FDEA02472.md): Frame · dented · Aug 13, 2004 · N246FE · Boeing 727200 · Fuselage Main, Frame
  > FWD CARGO COMPARTMENT FRAME DENTED STA 660 ABOVE STR 24L. REPAIRED BS 660 FRAME ST STR 24L IAW SRM 51-40-3 FIG 1.
- [SDR 04FDEA02471](https://openairdocs.org/sdr/04FDEA02471.md): Frame · dented · Aug 13, 2004 · N246FE · Boeing 727200 · Fuselage Main, Frame
  > FWD CARGO COMPARTMENT FRAME DENTED STA 520 BETWEEN STR 24L AND 25L. REPAIRED FRAME AT BS 520 BETWEEN STR 29L AND 25L IAW SRM 51-40-3 AND EA 7-5310- 70673.
- [SDR 04FDEA02470](https://openairdocs.org/sdr/04FDEA02470.md): Frame · dented · Aug 13, 2004 · N246FE · Boeing 727200 · Fuselage Main, Structure
  > FWD CARGO COMPARTMENT FRAME DENTED STA 520 BETWEEN STR 22L AND 23L. REPAIRED FRAME AT BS 520 BETWEEN STR 22L AND 23L IAW SRM 51-40-3 AND EA 7-5310- 70673.
- [SDR 04FDEA02469](https://openairdocs.org/sdr/04FDEA02469.md): Frame · dented · Aug 13, 2004 · N246FE · Boeing 727200 · Fuselage Main, Frame
  > FWD CARGO COMPARTMENT FRAME DENTED STA 500 BETWEEN STR 22L AND 23L. *S/D* REMOVED DAMAGE AREA OF FRAME BS 500 FABRICATED, ALODINED, PRIMED AND INSTALLED REPAIR IAW SRM 51-40-3.
- [SDR 04FDEA02468](https://openairdocs.org/sdr/04FDEA02468.md): Stringer · cracked · Aug 13, 2004 · N246FE · Boeing 727200 · Fuselage Main, Longeron/Stringer
  > CRACKED STRINGER 15 RT BS 720B 4 INCHES. *S/D* REPAIRED STR 15R AT BS 720B 4 INCHES PER SRM 53-10-3.
- [SDR 04FDEA02467](https://openairdocs.org/sdr/04FDEA02467.md): Stringer · cracked · Aug 13, 2004 · N246FE · Boeing 727200 · Fuselage Main, Longeron/Stringer
  > CRACKED STRINGER 15 LT AT BS 720B 4 INCHES. *S/D* REPAIRED STR 15L, BS 720B 4 INCHES IAW SRM 53-10-3.
- [SDR 04FDEA02460](https://openairdocs.org/sdr/04FDEA02460.md): Angle · corroded · Aug 12, 2004 · N246FE · Boeing 727200 · Fuselage Miscellaneous Structure
  > N00734 CORROSION ON FWD CARGO COMPARTMENT FLOOR SUPPORT WEB LOWER ANGLE STA 490 TO 500 LBL 9. REMOVED ANGLE AND FABRICATED, ALODINED AND PRIMED AND INSTALLED ANGLE IAW SRM 51-20-1, SRM 51-30-2, FED-EX MM 51-20-151-7
- [SDR 04FDEA02458](https://openairdocs.org/sdr/04FDEA02458.md): Keelbeam · corroded · Aug 12, 2004 · N246FE · Boeing 727200 · Fuselage Main, Keel
  > N00636 CORROSION, ON KEELBEAM STR 29L.950F 3 ON FLANGE AROUND FASTENER. ** SD COMING **
- [SDR 04FDEA02461](https://openairdocs.org/sdr/04FDEA02461.md): Stringer · corroded · Aug 12, 2004 · N246FE · Boeing 727200 · Fuselage Main, Longeron/Stringer
  > CORROSION FOUND WHILE WORKING NRC NR00286 FOUND CORRODED STR 30 AT BS 1084 BL 0. REPAIRED STR 30 AT BS 1084 IAW SRM 53-10-3
- [SDR 04FDEA02459](https://openairdocs.org/sdr/04FDEA02459.md): Keelbeam · corroded · Aug 12, 2004 · N246FE · Boeing 727200 · Fuselage Main, Keel
  > CORROSION ON KEELBEAM STR 29L, 950F+9 ON FLANGE AROUND HILOCK. CORROSION ON LT KEELBEAM BS 950F+9, FOUND TO BE OUT OF LIMITS. IAW SRM 53-10-1. REPAIRED IAW MM 27-53-013.
- [SDR 04FDEA02457](https://openairdocs.org/sdr/04FDEA02457.md): Keelbeam · corroded · Aug 12, 2004 · N246FE · Boeing 727200 · Fuselage Main, Keel
  > CORROSION ON RT KEELBEAM, STR 29 RT, BS 950D+15. CORROSION ON RT KEEL BEAM BS 950D15, FOUND TO BE OUT OF LIMITS IAW SRM 53-10-1.
- [SDR 04FDEA02456](https://openairdocs.org/sdr/04FDEA02456.md): Keelbeam · corroded · Aug 12, 2004 · N246FE · Boeing 727200 · Fuselage Main, Keel
  > CORROSION ON RT KEELBEAM, STR 29 RT, BS 950D PLUS 8. CORROSION ON RT KEELBEAM BS 950D PLUS 8. FOUND TO BE OUT OF LIMITS IAW SRM 53-10-1. REPAIRED IAW FED-EX 27-53-023A.
- [SDR 04FDEA02454](https://openairdocs.org/sdr/04FDEA02454.md): Stringer · dented · Aug 11, 2004 · N246FE · Boeing 727200 · Fuselage Main, Longeron/Stringer
  > BS 848 STR 7R UPPER FLANGE OF STRINGER IS DENTED. *S/D* REMOVED DAMAGE AREA OF STRINGER 7 RT AT BS 848, FABRICATED, ALODINE, PRIMED AND INSTALLED REPAIR IAW SRM 53-10-3 & PER FED EX EA 7-5310-55358.
- [SDR 04FDEA02453](https://openairdocs.org/sdr/04FDEA02453.md): Stringer · dented · Aug 11, 2004 · N246FE · Boeing 727200 · Fuselage Main, Longeron/Stringer
  > BS 848 STR 7L UPPER FLANGE OF STRINGER IS DENTED AND GOUGED. *S/D* REMOVED DAMAGE AREA OF STRINGER AT BS 848, FABRICATED, ALODINED, PRIMED AND INSTALLED REPAIR IAW SRM 53-10-3 & FED EX EA 7-5310-55348.
- [SDR 04FDEA02451](https://openairdocs.org/sdr/04FDEA02451.md): Stringer · dented · Aug 11, 2004 · N246FE · Boeing 727200 · Fuselage Main, Longeron/Stringer
  > STRINGER DENTED AT BS 950C 18, STRINGER 7 LT. *S/D* REPAIRED STR 7L BS 950C PLUS 18 PER SRM 53-10-3 FIG 2 DETAIL 1 & FED EX EA 7-5310-55358.
- [SDR 04FDEA02450](https://openairdocs.org/sdr/04FDEA02450.md): Stringer · dented · Aug 11, 2004 · N246FE · Boeing 727200 · Fuselage Main, Longeron/Stringer
  > STRINGER DENTED AT BS 950F 18, STRINGER 7 LT. REPAIRED STR 7L BS 950F PLUS 18 PER SRM 53-10-3 FIG 3 DETAIL 1 & FED EX EA 7-5310-55358
- [SDR 04FDEA02449](https://openairdocs.org/sdr/04FDEA02449.md): Stringer · dented · Aug 11, 2004 · N246FE · Boeing 727200 · Fuselage Main, Longeron/Stringer
  > STRINGER DENTED AT BS 1088, STRINGER 7 RT. REPAIRED STR 7R BS 1088 PER SRM 53-10-3 FIG 2 DETAIL 1 & FED EX EA 7-5310-55358
- [SDR 04FDEA02448](https://openairdocs.org/sdr/04FDEA02448.md): Stringer · dented · Aug 11, 2004 · N246FE · Boeing 727200 · Fuselage Main, Longeron/Stringer
  > STRINGER DENTED AT BS 950F+18, STRINGER 7 RT ** SD COMING **.
- [SDR 04FDEA02447](https://openairdocs.org/sdr/04FDEA02447.md): Stringer · dented · Aug 11, 2004 · N246FE · Boeing 727200 · Fuselage Main, Longeron/Stringer
  > STRINGER DENTED AT BS 950C PLUS 18, STRINGER 7 RT. REPAIRED STR 7R. BS 950C PLUS 18 PER SRM 53-10-3 FIG 2 DETAIL 1 & FED EX EA 7-5310-55358
- [SDR 04FDEA02446](https://openairdocs.org/sdr/04FDEA02446.md): Stringer · dented · Aug 11, 2004 · N246FE · Boeing 727200 · Fuselage Main, Longeron/Stringer
  > DENTED STRINGER 7R, BS 558. REPAIRED STR 7R BS 558 PER SRM 53-10-3 FIG 2 & FED EX EA 7-5310-55358
- [SDR 04FDEA02444](https://openairdocs.org/sdr/04FDEA02444.md): Stringer · dented · Aug 11, 2004 · N246FE · Boeing 727200 · Fuselage Main, Longeron/Stringer
  > DENTED STRINGER 7R BS678. REPAIRED STR. 7R AT BS 678 PER SRM 53-10-3 FIG 2 & FED EX EA 7-5310-55358
- [SDR 04FDEA02443](https://openairdocs.org/sdr/04FDEA02443.md): Stringer · dented · Aug 11, 2004 · N246FE · Boeing 727200 · Fuselage Main, Longeron/Stringer
  > DENTED STRINGER 7R BS 720C PLUS 18 INCHES. REPAIRED STR 7R, BS 720C PLUS 18 PER SRM 53-10-3 FIG 3 DETAIL I & FED EX EA 7-5310-55358
- [SDR 04FDEA02442](https://openairdocs.org/sdr/04FDEA02442.md): Stringer · dented · Aug 11, 2004 · N246FE · Boeing 727200 · Fuselage Main, Longeron/Stringer
  > DENTED STRINGER 7L BS 720E PLUS 18 INCHES. REPAIRED STR 7L, BS 720E PLUS 18 PER SRM 53-10-3 FIG 2. DETAIL I & FED EX EA 7-5310-55358
- [SDR 04FDEA02445](https://openairdocs.org/sdr/04FDEA02445.md): Stringer · dented · Aug 11, 2004 · N246FE · Boeing 727200 · Fuselage Main, Longeron/Stringer
  > DENTED STRINGER 7R BS618. TRIMMED OUT DAMAGE IAW SRM 53-10-1
- [SDR 04FDEA02452](https://openairdocs.org/sdr/04FDEA02452.md): Stringer · dented · Aug 11, 2004 · N246FE · Boeing 727200 · Fuselage Main, Longeron/Stringer
  > STRINGER DENTED AT BS 950 18, STRINGER 7 LT. *S/D* STR 7 LT ORIGINALLY FOUND OUT OF LIMITS (NO DENTS ALLOWED). REMOVED DENT BY BENDING EDGE OF STRINGER. MATERIAL LOSS A AS ALLOWABLE & STRINGER IS IN LIMITS PER SRM 53-10-1. ALODINED & PRIMED BLEND AREA PER
- [SDR 04FDEA02455](https://openairdocs.org/sdr/04FDEA02455.md): Floorbeam · corroded · Aug 11, 2004 · N246FE · Boeing 727200 · Fuselage Main, Floor Beam
  > CORROSION (C53-224-01, 1) FLOORBEAM STRUCTURE BS 344 LBL 31 TO LBL 58 WL 208. *S/D* REMOVED AND REPLACED UPPER FLOORBEAM CHORD AND REPAIR ANGLES AT BS 344, LBL 65-RBL 16, WL 208 IAW SRM 27-53-007.
- [SDR 04FDEA02417](https://openairdocs.org/sdr/04FDEA02417.md): Skin · corroded · Aug 10, 2004 · N246FE · Boeing 727200 · Fuselage Main, Plate/Skin
  > CORROSION BS 1090, STR 29 LT- 29 RT. CUTOUT SKIN AND INSTALLED REPAIR DOUBLER IAW SRM 53-30-3.
- [SDR 04FDEA02416](https://openairdocs.org/sdr/04FDEA02416.md): Skin · corroded · Aug 10, 2004 · N246FE · Boeing 727200 · Fuselage Main, Plate/Skin
  > CORROSION ON SKIN, AFT CARGO BAY BILGE NEXT TO O/B SIDE OF STR 28L BS 994 LBL 22 WL 136. REMOVED DAMAGED AREA OF SKINA T BS 994. FABRICATED AND INSTALLED REPAIR IAW SRM 53-30-3.
- [SDR 04FDEA02415](https://openairdocs.org/sdr/04FDEA02415.md): Floorbeam · corroded · Aug 10, 2004 · N246FE · Boeing 727200 · Fuselage Main, Floor Beam
  > CORROSION AT FLOORBEAM BS 950D, LBL 10 DAMAGED, WL 208 (C53-224-01, 3). BLENDED AREA AND FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. CUT OUT DAMAGE AND REPAIRED FLOORBEAM PER SRM 53-10-8 FIG 3.
- [SDR 03FDEA01132](https://openairdocs.org/sdr/03FDEA01132.md): Hydraulic Line · leaking · Jul 24, 2003 · N246FE · Boeing 727200 · Hydraulic System, Main
  > PASSING 17,000 FEET IN A NORMAL CLIMB BOTH HYDRAULIC SYSTEM "A" PUMP LOW PRESSURE LIGHTS CAME ON, FOLLOWED BY A COMPLETE LOSS OF SYSTEM "A" QUANITY. PERFORMED STABILIZERS EXECUTED CHECKLIST IAW QRH. DECLARED IFE AND LANDED UNEVENTFULLY AT IAH. INSTALLED NEW
- [SDR 02FDEA00423](https://openairdocs.org/sdr/02FDEA00423.md): Warning System · malfunctioned · Jun 21, 2002 · N246FE · Boeing 727200 · Engine Fuel Indicating System
  > FUEL HEAT ICING LIGHT ILLUMINATED ON ENG NR 3 APPROX 10-11000 MSL FOR ABOUT 1-2 MIN, THEN WENT OUT AND STAYED OUT. FUEL TEMP WAS +35DC. SUMPED ALL TANKS AND FOUND NO CONTAMINATION. FOUND FUEL FILTER PRESSURE SWITCH BACKSHELL EXTREMELY LOOSE AND WILL NEED TI
- [SDR 98FDEA00771](https://openairdocs.org/sdr/98FDEA00771.md): Actuator · malfunctioned · Dec 31, 1998 · N246FE · Boeing 727277 · Leading Edge Slat Actuator
  > WITH FLAPS RETRACT AS A/C ACCEL THRU 270 KIAS, AMBER LEAD EDGE LIGHT ILLUM ON 2ND OFFICER AUXILIARY PNL AND A/C ROLL CONTROL WAS AFFECTED. ANTI ICE WAS ON. BELOW 250 KIAS ALL IND WERE NORM, FLAP EXTENSION AND LAND, ALL APPROPRIATE CK LIST WERE COMPLETE. *S/

Next page: https://openairdocs.org/deregistered/N246FE-2009-07-28/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 = 'N246FE' AND deregistration_id = 'N246FE-2009-07-28'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N246FE-2009-07-28/reports

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