# Service difficulty reports: N107FE, cancelled Aug 10, 2006

A list on [N107FE, cancelled Aug 10, 2006](https://openairdocs.org/deregistered/N107FE-2006-08-10.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 · 55 reports

- [SDR 05FDEA02294](https://openairdocs.org/sdr/05FDEA02294.md): Channel · cracked · Aug 6, 2005 · N107FE · Boeing 727100 · Wing Miscellaneous Structure
  > RIGHT WING TRAILING EDGE AT AFT SPAR AREA 3 EA CLOSE OUT PANEL SUPPORTS ARE CRACKED LOCATED UNDER NR 12 & 13 SPOILER PANELS. REMOVED AND REPLACED 3 EACH CHANNEL SUPPORTS IAW SRM 51-30-2.
- [SDR 05FDEA00092](https://openairdocs.org/sdr/05FDEA00092.md): Rib · cracked · Jan 14, 2005 · N107FE · Boeing 727100 · Horizontal Stabilizer, Spar/Rib
  > STABILIZER-ELEVATOR HINGE SUPPORT RIB INSPEC - S/B 727-55A0091 R1 COMPLY WITH EO 7-5510-7-5001. FOUND CRACK IN RIB AT ELEVATOR STA 50.50 DURING INSPECTION IAW EO 7-5510-5001. REMOVED AND REPLACED RIB IAW EO 7-5510-5001.
- [SDR 04FDEA00216](https://openairdocs.org/sdr/04FDEA00216.md): Stiffener · corroded · Jan 24, 2004 · N107FE · Boeing 727100 · Fuselage Miscellaneous Structure
  > LEFT WHEEL WELL BULKHEAD STA 950 LOWER -TEE CHORD IS CORRODED. REMOVED AND REPLACED CHORD IAW SRM 51-30-2 ON N/R N00126 WO 24581 AT MAE.
- [SDR 04FDEA00214](https://openairdocs.org/sdr/04FDEA00214.md): Skin · corroded · Jan 23, 2004 · N107FE · Boeing 727100 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN BULGE AT STA 1163 STRINGER 18L & 19L. REMOVED CORROSION IAW SRM 51-10-6, FABRICATED & INSTALLED REPAIR DOUBLER IAW EA 7-5330-73867A.
- [SDR 04FDEA00202](https://openairdocs.org/sdr/04FDEA00202.md): Intercostal · damaged · Jan 22, 2004 · N107FE · Boeing 727100 · Fuselage Miscellaneous Structure
  > AFT PIT BS 1080 TO 1050 AT STR 26R INTERCOSTAL DAMAGED AND HOLES ELONGATED. REMOVED AND REPLACED INTERCOSTAL IAW SRM 51-30-2. NEW INTERCOSTAL FABRICATED ON TRAVELER NR T4/398010.
- [SDR 04FDEA00184](https://openairdocs.org/sdr/04FDEA00184.md): Support Angle · cracked · Jan 16, 2004 · N107FE · Boeing 727100 · Fuselage Miscellaneous Structure
  > LOWER NOSE COMPT DOOR CUTOUT SUPPORT ANGLE IS CRACKED AT FS 203 RBL 11. REMOVED AND REPLACED SUPPORT ANGLE IAW SRM 51-30-2 AT MAE ON N/R N00687.
- [SDR 04FDEA00183](https://openairdocs.org/sdr/04FDEA00183.md): Web · cracked · Jan 16, 2004 · N107FE · Boeing 727100 · Fuselage Main, Structure
  > UPPER DECK, CARGO DOOR UPPER BOX WEB FINGERS ARE CRACKED AT STA 490 AND 500 STR 2L. REMOVED DAMAGED WEB AND INSTALLED NEW WEB IAW SRM 51-30-2.
- [SDR 04FDEA00182](https://openairdocs.org/sdr/04FDEA00182.md): Seat Track · corroded · Jan 16, 2004 · N107FE · Boeing 727100 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN SEAT TRACK AT APPROX RBL 24 FS 1140 TO 1183 IS CORRODED. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-30-2 AT MAE ON N/R N00448.
- [SDR 04FDEA00181](https://openairdocs.org/sdr/04FDEA00181.md): Floor Support · cracked · Jan 16, 2004 · N107FE · Boeing 727100 · Fuselage Miscellaneous Structure
  > AFT LOWER PIT BS 970 TO 990 BETWEEN STR 29 AND LT KEEL BEAM CRACKED FLOOR SUPPORT AND CORRODED NUT PLATES. REMOVED AND REPLACED FLOOR SUPPORT IAW SRM 53-10-5 AT MAE ON N/R NOO419.
- [SDR 03FDEA02208](https://openairdocs.org/sdr/03FDEA02208.md): Coupler · failed · Dec 16, 2003 · N107FE · Boeing 727100 · Auto Flight System
  > LOWER YAW DAMPER RUNAWAY - LT AND RT AFTER TAKEOFF - LYD SWITCH TURNED OFF. REMOVED AND REPLACED LOWER YAW DAMP COUPLER IAW 727-100 MM CH 22-11-131-4. OPS CHECKS NORMAL ON GROUND. A/C OK FOR SERVICE.
- [SDR 03FDEA01408](https://openairdocs.org/sdr/03FDEA01408.md): Switch · false indication · Sep 3, 2003 · N107FE · Boeing 727100 · Landing Gear Position and Warning
  > NOSE GEAR DID NOT INDICATE SAFE AFTER PLACING LANDING GEAR HANDLE DOWN. CYCLED LANDING GEAR LEVER. NOSE GEAR INDICATED SAFE AFTER APPROX 10 - 15 SEC. RED UNSAFE WAS NOT ILLUMINATED. REMOVED AND REPLACED SWITCHES S93 AND S96 IAW M/M 32-61-021-4. OPS CK GOOD.
- [SDR 03FDEA00126](https://openairdocs.org/sdr/03FDEA00126.md): Coalescer Bag · contaminated · Feb 14, 2003 · N107FE · Boeing 727100 · Humidity Control System
  > AFTER GEAR RETRACTION, CREW BECAME AWARE OF AN ACRID ODOR WHICH INTENSIFIED. INITIAL ODOR WAS OF BURNING RUBBER OR A SMOLDERING WIRE BUNDLE. CREW WENT ON OXYGEN AND RETURNED TO IND. PERFORMED FIRE, SMOKE, FUMES AND ODOR CHECKLIST. REPLACED BOTH WATER S
- [SDR 02FDEA00703](https://openairdocs.org/sdr/02FDEA00703.md): Actuator · failed · Oct 2, 2002 · N107FE · Boeing 727100 · Leading Edge Slat Actuator
  > DURING FLAP RETRACTION NR 2 SLAT ON RIGHT WING REMAINED EXTENDED WITH FLAP LEVER IN UP POSITION. QRH PROCEDURES WERE FOLLOWED AND FLAPS WERE CYCLED BACK TO 5 ON SCHEDULE FLAPS RETRACTED AGAIN AND PROBLEM CONTINUED. REMOVED AND REPLACED NR 2 SLAT ACTUATOR AS
- [SDR 02FDEA00513](https://openairdocs.org/sdr/02FDEA00513.md): Oil Filter · damaged · Jul 23, 2002 · N107FE · Boeing 727100 · Engine Oil Indicating System
  > NR 1 ENGINE, HIGH OIL TEMP (OFF SCALE HIGH) FOUND BAD CONNECTION AT OIL TEMP SENSOR. PER CREW INFO WINDMILLING WAS LESS THAN 30 MIN. FOUND BROKEN WIRE AT C/P ON NR 1 ENG OIL TEMP BULB. REMOVED AND REPLACED C/P D530 IAW SWPM. PERFORMED ENGINE WINDMILLING IN
- [SDR 01FDEA00503](https://openairdocs.org/sdr/01FDEA00503.md): Skin · corroded · Jun 26, 2001 · N107FE · Boeing 72722C · Fuselage Main, Plate/Skin
  > N 371 DUR ROUTINE INSP FUSELAGE SKIN FND CORRODED FROM BS 425-440 BETWEEN STR 3L AND 4L. R&R & FAB SKIN PER IAW BAC 727 SRM 53-30-3.
- [SDR 01FDEA00502](https://openairdocs.org/sdr/01FDEA00502.md): Fitting · corroded · Jun 26, 2001 · N107FE · Boeing 72722C · Landing Gear Door Retract Section
  > N 773 DUR ROUTINE INSP, NLG DOOR UPR LINK FITTING BS 227.8 FND CORRODED. R&R FITTING IAW BAC 727 SRM 51-30-2.
- [SDR 01FDEA00453](https://openairdocs.org/sdr/01FDEA00453.md): Support · cracked · Jun 18, 2001 · N107FE · Boeing 72722C · Fuselage Miscellaneous Structure
  > DURING ROUTINE INSP THE NR 1 SEAT TRACK SUPPORT AT BS 860 FOUND CRACKED. *S/D* REMOVED AND REPLACED SUPPORT PER IAW BAC 727 SRM 51-30-2.
- [SDR 01FDEA00414](https://openairdocs.org/sdr/01FDEA00414.md): Pressure Panel · cracked · Jun 11, 2001 · N107FE · Boeing 72722C · Fuselage Main, Bulkhead
  > DURING ROUTINE INSP LT SIDE WEB IN NOSE WHEEL WELL WAS FOUND CRACKED AT BS 1260. *S/D* REMOVED, REPLACED AND FAB PER IAW BAC 727 SRM 51-20-1, 51-30-2.
- [SDR 01FDEA00413](https://openairdocs.org/sdr/01FDEA00413.md): Web · cracked · Jun 11, 2001 · N107FE · Boeing 72722C · Fuselage Miscellaneous Structure
  > DURING ROUTINE INSP, LT SIDE WEB IN AIRSTAIR COMPT FOUND CRACKED AT LIGHTENING HOLE AT BS 1263. *S/D* REMOVED, REPLACED AND FAB PER IAW BAC 727 SRM 51-40-2, 51-30-2.
- [SDR 01FDEA00412](https://openairdocs.org/sdr/01FDEA00412.md): Fitting · cracked · Jun 11, 2001 · N107FE · Boeing 72722C · Elevator Tab Control System
  > DURING ROUTINE INSP, RT ELEVATOR TAB ROD FITTING FOUND CRACKED. *S/D* REMOVED AND REPLACED RIGHT ELEVATOR TAB PER IAW BAC 727 MM 27-30-011-2.
- [SDR 01FDEA00401](https://openairdocs.org/sdr/01FDEA00401.md): Beam · cracked · Jun 11, 2001 · N107FE · Boeing 72722C · Fuselage Main, Bulkhead
  > DURING ROUTINE INSP BS 1183 BULKHEAD VERTICAL BEAM AT LBL 27 FOUND CRACKED AT WL 263. *S/D* REMOVED AND REPLACED PER VERTICAL BEAM PER IAW FEDEX EO 7-5310-7-2346 PART 2.
- [SDR 01FDEA00411](https://openairdocs.org/sdr/01FDEA00411.md): Web · cracked · Jun 11, 2001 · N107FE · Boeing 72722C · Fuselage Miscellaneous Structure
  > DURING ROUTINE INSP, RT SIDE WEB IN AFT AIRSTAIR AREA FOUND CRACKED AT BS 1283. *S/D* REMOVED, REPLACED AND FAB PER IAW BAC 727 BAC 727 SRM 51-40-2, 51-30-2.
- [SDR 01FDEA00410](https://openairdocs.org/sdr/01FDEA00410.md): Tie Clip · cracked · Jun 11, 2001 · N107FE · Boeing 72722C · Fuselage Miscellaneous Structure
  > DURING ROUTINE INSP, STR TIE CLIP AT BS 312, STR 4R FOUND CRACKED. *S/D* REMOVED, REPLACED AND FAB PER IAW BAC 727 SRM 51-20-1, 51-30-2.
- [SDR 01FDEA00409](https://openairdocs.org/sdr/01FDEA00409.md): Tie Clip · cracked · Jun 11, 2001 · N107FE · Boeing 72722C · Fuselage Miscellaneous Structure
  > DURING ROUTINE INSP, STR TIE CLIP AT BS 328, STR 14R FOUND CRACKED. *S/D* REMOVED, REPLACED AND FAB PER IAW BAC 727 SRM 51-20-1, 51-30-2.
- [SDR 01FDEA00408](https://openairdocs.org/sdr/01FDEA00408.md): Skin · cracked · Jun 11, 2001 · N107FE · Boeing 72722C · Emergency Exits
  > DURING ROUTINE INSP, LT FWD EMERGENCY EXIT HATCH UPPER INNER SKIN FOUND CRACKED. *S/D* REMOVED, REPLACED AND FAB PER IAW BAC 727 SRM 52-00-3, 51-30-2.
- [SDR 01FDEA00407](https://openairdocs.org/sdr/01FDEA00407.md): Bulkhead · cracked · Jun 11, 2001 · N107FE · Boeing 72722C · Fuselage Main, Bulkhead
  > DURING ROUTINE INSP, HFEC IND TWO CRACKS IN BS 1183 BULKHEAD WEB AT WL 283. *S/D* REMOVED AND REPLACED WEB PER IAW FEDEX EO 7-5310-7-5000 PARTS 2 & 4.
- [SDR 01FDEA00406](https://openairdocs.org/sdr/01FDEA00406.md): Bulkhead · cracked · Jun 11, 2001 · N107FE · Boeing 72722C · Fuselage Main, Bulkhead
  > DURING ROUTINE INSP, HFEC IND CRACK IN BS 1183 BULKHEAD WEB AT WL 283, RBL 17.8. *S/D* REMOVED AND REPLACED PER IAW FEDEX EO 7-5310-7-5000 PARTS 3 & 5.
- [SDR 01FDEA00405](https://openairdocs.org/sdr/01FDEA00405.md): Fitting · cracked · Jun 11, 2001 · N107FE · Boeing 72722C · Fuselage Miscellaneous Structure
  > DURING ROUTINE INSP, HFEC IND CRACK IN FASTENER HOLES IN ROW 3, LT BS 870 FITTING AT STR 9L. *S/D* HFEC IND NO CRACKS PER IAW BAC 727 NDT MANUAL PART 6.
- [SDR 01FDEA00404](https://openairdocs.org/sdr/01FDEA00404.md): Floorbeam · cracked · Jun 11, 2001 · N107FE · Boeing 72722C · Fuselage Main, Floor Beam
  > DURING ROUTINE INSP FLT DECK FLOORBEAM WEB AT BS 299, LBL 6 FOUND CRACKED. *S/D* REMOVED, REPLACED AND FAB WEB PER IAW BAC 727 SRM 51-20-1, SRM 51-30-2.
- [SDR 01FDEA00403](https://openairdocs.org/sdr/01FDEA00403.md): Rib · cracked · Jun 11, 2001 · N107FE · Boeing 72722C · Rudder, Spar/Rib
  > DURING ROUTINE INSP LWR RUDDER, LWR THRUST HINGE RIB FOUND CRACKED AT FASTENER COMMON TO FIN REAR SPAR. *S/D* HFEC IND CRACK TERMINATED. REMOVED, REPLACED AND FAB PER IAW FEDEX DRAWING SRM 27-55-005, SRM 51-30-2.
- [SDR 01FDEA00402](https://openairdocs.org/sdr/01FDEA00402.md): Support · cracked · Jun 11, 2001 · N107FE · Boeing 72722C · Fuselage Miscellaneous Structure
  > DURING ROUTINE INSP THE NR 1 SEAT TRACK SUPT AT BS 840 FOUND CRACKED.
- [SDR 99FDEA00053](https://openairdocs.org/sdr/99FDEA00053.md): Battery · discharged · Feb 2, 1999 · N107FE · Boeing 72722C · Emergency Lighting
  > ENTRY DOOR EMERGENCY LIGHT BURNED OUT. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK ON FORWARD ENTRY DOOR. SYS OPER CK GOOD IAW FEDEX MM 33-50-0.
- [SDR 98FDEA00726](https://openairdocs.org/sdr/98FDEA00726.md): Pump · failed · Dec 5, 1998 · N107FE · Boeing 72722C · Turbine Engine Oil System
  > DURING CLIMBOUT, NR 2 LOW OIL PRESS/FILTER BYPASS LIGHT CAME ON. OIL PRESS DROPPED TO ZERO, TEMP WAS OK. SHUTDOWN ENG PER RED TABS WITHIN 4 TO 5 MIN. *S/D* REMOVED AND REPLACED NR 2 ENG OIL PUMP.
- [SDR 96FDEA01550](https://openairdocs.org/sdr/96FDEA01550.md): Hyd Line · cracked · Sep 26, 1996 · N107FE · Boeing 72722 · Hydraulic System, Main
  > IN-FLIGHT AT FL 280, NR 1 ENGINE HYDRAULIC PUMP LIGHT STARTED BLINKING WITH FLUCTUATION IN PRESSURE. TWO SECONDS LATER, NR 2 ENGINE HYD PRESS LIGHT BLINKED, THEN BOTH LIGHTS CAME ON STEADY WITH RAPID LOSS OF ALL A-SYSTEM HYD FLUID. PUMPS WERE OPERATED WITHOU
- [SDR 96FDEA01432](https://openairdocs.org/sdr/96FDEA01432.md): Track · corroded · Sep 3, 1996 · N107FE · Boeing 72722C · Fuselage Miscellaneous Structure
  > CORROSION ON O/B OF TRACK STA 840 RBL 48. INSTALLED DOUBLER PER EA 7531-0-28823 AND 51-10-1.
- [SDR 96FDEA01426](https://openairdocs.org/sdr/96FDEA01426.md): Integral Rib · cracked · Aug 22, 1996 · N107FE · Boeing 727233 · Fuselage Miscellaneous Structure
  > LT 870 INTEGRAL RIB FWD CRACK FROM O/B HOLE TO EDGE. INSTALLED BATHTUB FITTING PER EA NR 7-5310-28832.
- [SDR 96FDEA01430](https://openairdocs.org/sdr/96FDEA01430.md): Skin · corroded · Aug 21, 1996 · N107FE · Boeing 72722C · Wing, Plate/Skin
  > UPPER SURFACE CENTER WING SECTION, CENTER WING SKIN HAS HEAVY CORROSION AT LT AFT CORNER SECTION UNDER PRESS. SEAL TRACK APPROX 6 INCH AREA, THREE PLACES FS 850 TO 856. CORROSION REMOVED, DIGITAL THICKNESS CHECKED BY NDT, ORIG 184 TAKEN DOWN TO.068. REPAIR
- [SDR 96FDEA01428](https://openairdocs.org/sdr/96FDEA01428.md): Angle · corroded · Aug 15, 1996 · N107FE · Boeing 72722C · Fuselage Miscellaneous Structure
  > FLOOR BOARD SUPPORT ANGLE CORRODED AT STA 344 26 TO 45 LBL FLOOR BEAM. REMOVED CORROSION AND INSTALLED CAP STRIP REPAIR PER SRM 51-10-1.
- [SDR 96FDEA01431](https://openairdocs.org/sdr/96FDEA01431.md): Angle · corroded · Aug 14, 1996 · N107FE · Boeing 72722C · Fuselage Miscellaneous Structure
  > CABIN INTERIOR, FS 1176 REINFORCEMENT CHORD ANGLE HAS HEAVY TO SEVERE CORROSION. FLOOR LEVEL BETWEEN BL 44 TO 46 LT. REMOVED DAMAGED PORTION OF CHORD ANGLE, INSTALLED NEW SECTION AND SPLICE DOUBLER PER E/A NR 7531028817.
- [SDR 96FDEA01429](https://openairdocs.org/sdr/96FDEA01429.md): Seat Track · corroded · Aug 14, 1996 · N107FE · Boeing 72722C · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON O/B OF TRACK STA 840 RBL 48. INSTALLED DOUBLER PER EA 7531028823.
- [SDR 96FDEA01427](https://openairdocs.org/sdr/96FDEA01427.md): Splice Plate · corroded · Aug 14, 1996 · N107FE · Boeing 72722C · Fuselage Miscellaneous Structure
  > CORROSION UNDER WING TO FUSE SPLICE PLATE LT SIDE AFT CORNER OF TANK BS 870 LBL 70.5. CUT OUT CORROSION, INSTALLED REPAIR PER EA 7-5710-28845.
- [SDR 96FDEA01361](https://openairdocs.org/sdr/96FDEA01361.md): Doubler · cracked · Aug 13, 1996 · N107FE · Boeing 72722C · Fuselage Miscellaneous Structure
  > FOUND CRACK AT FWD ENTRY DOOR CUT OUT FRAME UPPER HINGE AREA. INSTALLED DOUBLER AS PER SRM 53-10-4 FIG 2.
- [SDR 96FDEA01360](https://openairdocs.org/sdr/96FDEA01360.md): Flange · corrosion · Aug 13, 1996 · N107FE · Boeing 72722C · Fuselage Miscellaneous Structure
  > NR0176, MAIN CARGO HAS CORR ON STR 5L STA 1148 TO 1166. REMOVED CORR SRM 51-10-6 OUT OF LIMITS, CUT REPAIR PARTS FOR INSIDE FLANGE REPAIR PER SRM 53-10-3.
- [SDR 96FDEA1359](https://openairdocs.org/sdr/96FDEA1359.md): Doubler · cracked · Aug 12, 1996 · N107FE · Boeing 72722C · Fuselage Miscellaneous Structure
  > RT 870 INTERGRAL RIB FWD CRACKED FROM O/B HOLE TO EDGE. THE 2ND CRACK O/B OF O/B HOLE CRACKED FROM EDGE THROUGH RADIUS INTO AFT LWR HOLE OF O/B FLANGE. INSTALLED DOUBLER PER EZ 7-5310-28831.
- [SDR 96FDEA01353](https://openairdocs.org/sdr/96FDEA01353.md): Floor Beam · corrosion · Aug 12, 1996 · N107FE · Boeing 72722C · Fuselage Main, Floor Beam
  > MAIN CARGO CORROSION ON FLOOR BEAM AT STA 312 LBL 19. INSTALLED AND COMPLETED FLOOR BEAM REPAIR STA 312 LBL 19 PER SRM 53-10-8.
- [SDR 96FDEA01352](https://openairdocs.org/sdr/96FDEA01352.md): Stringer · corroded · Aug 12, 1996 · N107FE · Boeing 72722C · Fuselage Main, Longeron/Stringer
  > FORWARD CARGO BS 720 STR 23R HEAVY CORROSION INSIDE STRINGER ON LOWER LEG. REMOVED CORROSION AND INSTALLED STRINGER REPAIR PER SRM 53-10-3.
- [SDR 96FDEA01338](https://openairdocs.org/sdr/96FDEA01338.md): Window Post · cracked · Aug 7, 1996 · N107FE · Boeing 72722C · Fuselage Miscellaneous Structure
  > CRACK AT F/O'S NR 1 WINDOW O/B POST AT UPPER CORNER. CRACK LENGTH VERIFIED BY NDT HFEC, CRACK WAS STOP DRILLED AND VERIFIED BY NDT HFEC REPAIR DOUBLER INSTALLED PER SRM 53-30-3.
- [SDR 96FDEA01318](https://openairdocs.org/sdr/96FDEA01318.md): Stringer · corrosion · Aug 4, 1996 · N107FE · Boeing 72722C · Fuselage Main, Longeron/Stringer
  > NR0440, FWD CARGO BS 720 STR 23R HEAVY CORROSION INSIDE STR ON LOWER LEG. *S/D* REMOVED CORROSION AND INSTALLED STRINGER REPAIR PER 53-10-3.
- [SDR 96FDEA01317](https://openairdocs.org/sdr/96FDEA01317.md): Floor Beam · corrosion · Aug 2, 1996 · N107FE · Boeing 72722C · Fuselage Main, Floor Beam
  > NR0436, FWD CARGO BS 600 BL 0 TO RBL 24 HEAVY CORROSION ON LOWER SIDE OF LOWER LEG OF MAIN CARGO FLOOR BEAM. *S/D* INSTALLED FLOOR BEAM REPAIR PER SRM 53-10-8.
- [SDR 96FDEA01314](https://openairdocs.org/sdr/96FDEA01314.md): Fitting · cracked · Aug 2, 1996 · N107FE · Boeing 72722C · Fuselage Miscellaneous Structure
  > STR END FITTING CRACKED STA 740 STR 5R. REMOVED AND REPLACED STR END FITTING PER 51-10-01.

Next page: https://openairdocs.org/deregistered/N107FE-2006-08-10/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 = 'N107FE' AND deregistration_id = 'N107FE-2006-08-10'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N107FE-2006-08-10/reports

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