# Service difficulty reports: N407DA, cancelled Jan 31, 2001

A list on [N407DA, cancelled Jan 31, 2001](https://openairdocs.org/deregistered/N407DA-2001-01-31.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 · 51 reports

- [SDR DL72S002028](https://openairdocs.org/sdr/DL72S002028.md): Engine · bird strike · Oct 16, 2000 · N407DA · Boeing 727232 · Engine (Turbine/Turboprop)
  > DURING TAKEOFF, A/C SUFFERED BIRD STRIKE, FODDING OUT NR 1 ENGINE. REPLACED ENGINE.
- [SDR DL72S001699](https://openairdocs.org/sdr/DL72S001699.md): Light · inoperative · Sep 3, 2000 · N407DA · Boeing 727232 · Emergency Lighting
  > ON L/O, FOUND L-2 OVER DOOR EMERGENCY LIGHT INOP. REPLACED LIGHT ASSY.
- [SDR DL72S001169](https://openairdocs.org/sdr/DL72S001169.md): Battery · discharged · Jun 16, 2000 · N407DA · Boeing 727232 · Emergency Lighting
  > AFT CABIN DOOR OVERHEAD EMERG LIGHT INOP. C/W REPLACED BATTERIES, OPS NOW OK.
- [SDR DL72S000300](https://openairdocs.org/sdr/DL72S000300.md): Engine · failed · Feb 13, 2000 · N407DA · Boeing 727232 · Engine (Turbine/Turboprop)
  > RIGHT ENGINE OIL PRESS HIGH WITH NR 3 OIL BYPASS LIGHT. ENGINE SUBSEQUENTLY FAILED. REPLACED ENGINE.
- [SDR DL72S992706](https://openairdocs.org/sdr/DL72S992706.md): Bracket · cracked · Dec 10, 1999 · N407DA · Boeing 727232 · Leading Edge Slat Actuator
  > A 1.25 INCH CRACK NR 8 SLAT ACTUATOR I/B AFT ATTACH BRACKET. REPAIRED PER MM 57-20-21.
- [SDR DL72S992688](https://openairdocs.org/sdr/DL72S992688.md): Light · inoperative · Dec 9, 1999 · N407DA · Boeing 727232 · Flight Compartment Lighting
  > FLIGHT DECK EMERGENCY PORTABLE EXIT IDENTIFIER LIGHT WOULD NOT TEST. REPLACED BATTERY PACK, OP CKS GOOD.
- [SDR DL72S991433](https://openairdocs.org/sdr/DL72S991433.md): Skin · cracked · Jun 23, 1999 · N407DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > LFEC INSPECTION OF THE STRINGER 26L SKIN LAP SPLICE BETWEEN FS 481 & 681 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED 5 CRACKS ALONG THE JOINT. THE SKIN LAP WAS CUTOUT ALONG THE ENTIRE PANEL LENGTH AND REPA
- [SDR DL72S991178](https://openairdocs.org/sdr/DL72S991178.md): Csd · required service · May 25, 1999 · N407DA · Boeing 727232 · Alternator-Generator Drive
  > CSD LOW PRESSURE LIGHT FLICKERED AND THEN STAYED ON, LOST MAIN AC NR 2. FOUND CSD LOW. SERVICED CSD, RAN ENG AND NO LEAKS NOTED.
- [SDR DL72S991124](https://openairdocs.org/sdr/DL72S991124.md): Web · cracked · May 20, 1999 · N407DA · Boeing 727232 · Fuselage Miscellaneous Structure
  > TPA LTR CHK B-2, LT VERT TORQUE BOX WEB CRACKED.25 INCH AT UPPER LIGHTENING HOLE AT STA 1226. REPAIRED PER MM 53-11-0 PG 828, LT VERT TORQUE BOX WEB LWR LIGHTENING HOLE.375 INCH CRACK AT UPPER END AND A.625 INCH CRACK ON LWR END STA 1226. REPAIRED PER MM
- [SDR DL72S991122](https://openairdocs.org/sdr/DL72S991122.md): Frame · cracked · May 20, 1999 · N407DA · Boeing 727232 · Fuselage Miscellaneous Structure
  > FOUND AT B-2 LETTER CHECK, LT AFT ENTRYWAY DOOR FRAME HAS.375 INCH VISIBLE CRACK. REPAIRED PER SRM 53-10-9.
- [SDR DL72S990588](https://openairdocs.org/sdr/DL72S990588.md): Skin · cracked · Mar 15, 1999 · N407DA · 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 8 CRACKS ALONG THE PANEL LENGTH. THE SKIN LAP WAS CUT OUT ALONG THE PANEL LENGTH AND RE
- [SDR DL72S990546](https://openairdocs.org/sdr/DL72S990546.md): Skin · cracked · Mar 13, 1999 · N407DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > LFEC INSPECTION OF THE STRINGER 26L SKIN LAP SPLICE BETWEEN FS 360 AND 680 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. HFEC INTERNAL INSPECTION CONFIRMED 3 CRACKS BETWEEN FS 500 AND 520. THE CRACKS WERE ROUTED OUT OF THE SKIN LAP AND REPAIR
- [SDR DL72S990566](https://openairdocs.org/sdr/DL72S990566.md): Skin · cracked · Mar 11, 1999 · N407DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > LFEC INSPECTION OF THE STRINGER 4L SKIN LAP SPLICE BETWEEN FS 360 AND 480 INDICATED A CRACK IN LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED 3 CRACKS BETWEEN FS 400 AND 420. THE CRACKS WERE CUT OUT AND REPAIRED PER B727 SRM 53-30-3
- [SDR DL72S990565](https://openairdocs.org/sdr/DL72S990565.md): Skin · cracked · Mar 11, 1999 · N407DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 680 TO 740 INDICATED A CRACK IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED A SINGLE CRACK BETWEEN FS 720 AND 720A. THE CRACKED AREA WAS ROUTED OUT AND REPAIRED PE
- [SDR DL72S990562](https://openairdocs.org/sdr/DL72S990562.md): Skin · cracked · Mar 11, 1999 · N407DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 360 AND 481 REVEALED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED 3 CRACKS BETWEEN FS 360 AND 380. THE CRACKS WERE ROUTED OUT AND REPAIRED PER B727 SRM
- [SDR DL72S990348](https://openairdocs.org/sdr/DL72S990348.md): Pump · failed · Feb 21, 1999 · N407DA · Boeing 727232 · Hydraulic Pump (Electric/Engine), Main
  > B-SYSTEM HYD WENT TO 0, FOLLOWED PROCEDURES. WHEN GEAR EXTENDED HYD PRESS WENT TO 1700 PSI. OPERATED BRAKE INTERCONNECT, USED PNEUMATIC BRAKES TO STOP. TOWED ACFT TO GATE FROM RUNWAY. FOUND NR 2 B-HYD PUMP LEAKING. REPLACED SAME AND FITTINGS, LEAK CKS OK.
- [SDR DL72S982564](https://openairdocs.org/sdr/DL72S982564.md): Actuator · leaking · Dec 15, 1998 · N407DA · Boeing 727232 · Leading Edge Slat Actuator
  > AIRCRAFT LOST 'A SYSTEM HYDRAULICS WHILE TAXING TO THE GATE AFTER LANDING IN CVG. MTC FOUND THAT THE NUMBER 7 LEADING EDGE SLAT ACTUATOR HAD FAILED. REPLACED ACTUATOR AND BOTH HYDRAULIC PUMPS.
- [SDR DL72S982154](https://openairdocs.org/sdr/DL72S982154.md): Stringer · cracked · Oct 16, 1998 · N407DA · Boeing 727232 · Wing, Longeron/Stringer
  > S18 TAB ON THE RT WING VENT BOX AT WS 171.5 WAS FOUND CRACKED. ADDITIONAL DAMAGE INCURRED WHILE INSTALLING THE SRM REPAIR. REPAIRED PER ERA 332288-14.
- [SDR DL72S982151](https://openairdocs.org/sdr/DL72S982151.md): Stringer · cracked · Oct 16, 1998 · N407DA · Boeing 727232 · Fuselage Main, Longeron/Stringer
  > FUSE STR 29R WAS FOUND CRACKED AT FS 950E. REPAIRED PER ERA 332275-14.
- [SDR DL72S982150](https://openairdocs.org/sdr/DL72S982150.md): Stringer · cracked · Oct 16, 1998 · N407DA · Boeing 727232 · Wing, Longeron/Stringer
  > RT WING UPPER SURFACE S18 AT WS 304 WAS FOUND CRACKED, REQUIRING A 2.5 INCH CUTOUT. REPAIRED PER ERA 332341-14.
- [SDR DL72S982149](https://openairdocs.org/sdr/DL72S982149.md): Frame · cracked · Oct 16, 1998 · N407DA · Boeing 727232 · Wing Spar
  > CRACK WAS FOUND IN THE VERT FLANGE OF THE WING TO FUSE UPPER ATTACH CHORD, LWR FRAME HOLE RBL 70.85, FS 760. REPAIRED PER ERA 332283-14AD.
- [SDR DL72S982139](https://openairdocs.org/sdr/DL72S982139.md): Skin · cracked · Oct 14, 1998 · N407DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN WAS FOUND WITH A TIME LIMITED EXT REPAIR DOUBLER FOR A CRACK IN THE SKIN AT FS 294.5, BELOW S15R. THE TIME LIMITED REPAIR WAS REMOVED AND ADDITIONAL DAMAGE FOUND. REPAIRED PER ERA 332347-14.
- [SDR DL72S982094](https://openairdocs.org/sdr/DL72S982094.md): Skin · cracked · Oct 8, 1998 · N407DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > FUSE SKIN HAD A TIME LIMITED REPAIR REMOVED AT FS294, S15R; AND ADDITIONAL DAMAGE WAS FOUND. REPAIRED PER ERA 332347-14.
- [SDR DL72S982085](https://openairdocs.org/sdr/DL72S982085.md): Spar · damaged · Oct 8, 1998 · N407DA · Boeing 727232 · Wing Spar
  > DURING INSPECTION OF THE CTR WING REAR SPAR AND REPAIR MANY FASTENER LOCATIONS IN THE SPAR PANEL WERE OVERSIZED DUE TO TOOLING DAMAGE. REPAIRED PER ERA 332359-14AD.
- [SDR DL72S982063](https://openairdocs.org/sdr/DL72S982063.md): Frame · cracked · Oct 6, 1998 · N407DA · Boeing 727232 · Fuselage Main, Frame
  > A CRACK WAS FOUND IN THE FS 784 RT FRAME INBD FLANGE. THE CRACK PROPAGATES FROM THE FIRST FASTENER HOLE ABOVE THE FLOOR LINE. REPAIRED PER ERA 300891-14AD, REV A.
- [SDR DL72S982112](https://openairdocs.org/sdr/DL72S982112.md): Track · corroded · Oct 1, 1998 · N407DA · Boeing 727232 · Trailing Edge Flaps
  > CORROSION FOUND AT FWD ATTACH LUG FACES AND BORE AND TO MLG BEAM ATTACH HOLES. BUSH LUG HOLES AND INSTALLED SPLICE PLATE REPAIR FOR MLG BEAM ATTACH HOLES.
- [SDR DL72S982318](https://openairdocs.org/sdr/DL72S982318.md): Angle · cracked · Sep 30, 1998 · N407DA · Boeing 727232 · Trailing Edge Flaps
  > DURING SHOP INSPECTION, THE AFT CHORD ANGLE WAS FOUND CRACKED 18 INCHES FROM I/B END OF FLAP. THE ANGLE WAS REPAIRED PER MM 57-52-0 FIG 802 BY REPLACING A SECTION OF THE ANGLE AND INSTALLING A SPLICE DOUBLER.
- [SDR DL72S982316](https://openairdocs.org/sdr/DL72S982316.md): Skin · cracked · Sep 30, 1998 · N407DA · Boeing 727232 · Trailing Edge Flaps
  > DURING SHOP INSPECTION, THE COVE SKIN WAS FOUND CRACKED 34 INCHES FROM I/B END OF FLAP. THE SKIN WAS REPAIRED PER MM 57-52-0, FIG 809 BY REMOVING THE DAMAGE AND INSTALLING A DOUBLER.
- [SDR DL72S982315](https://openairdocs.org/sdr/DL72S982315.md): Angle · repaired · Sep 30, 1998 · N407DA · Boeing 727232 · Trailing Edge Flaps
  > DURING SHOP INSPECTION, THE AFT CHORD ANGLE WAS FOUND CRACKED AT 2 PLACES APPROX 34 INCHES FROM I/B END OF FLAP. THE ANGLE WAS REPAIRED PER MM 57-52-00, FIG 802 BY REPLACING A SECTION OF THE ANGLE AND INSTALLING A SPLICE DOUBLER.
- [SDR DL72S982053](https://openairdocs.org/sdr/DL72S982053.md): Rib · cracked · Sep 29, 1998 · N407DA · Boeing 727232 · Trailing Edge Flaps
  > INBOARD AFT CLOSE OUT RIB CRACKED AT LWR AFT CORNER. DAMAG REPAIRED PER MM 57-52-0 ON SHOP ORDER 582612.
- [SDR DL72S981998](https://openairdocs.org/sdr/DL72S981998.md): Pin · corroded · Sep 25, 1998 · N407DA · Boeing 727232 · Fuselage Miscellaneous Structure
  > BORE CORRODED LEFT AFT BTL PIN IS CORRODED. CLEANED CORROSION PER SRM 53-40-1 FIG 4 DAMAGE WITHIN LIMITS OK TO TREAT. TREATED BORE PER PS 900-2-4-1 NO O2.
- [SDR DL72S982218](https://openairdocs.org/sdr/DL72S982218.md): Angle · cracked · Sep 23, 1998 · N407DA · Boeing 727232 · Trailing Edge Flaps
  > DURING SHOP VISIT THE AFT LOWER CHORD ANGLE WAS FOUND CRACKED 21 AND 34 FR OM IB END OF FLAP. THE ANGLE WAS REPAIRED BY SPLICING IN A NE W SECTION OF ANGLEPER MM 57-52-0, FIG. 802.
- [SDR DL72S982060](https://openairdocs.org/sdr/DL72S982060.md): Support · worn · Sep 23, 1998 · N407DA · Boeing 727232 · Fuselage Miscellaneous Structure
  > ITEM: NR 2 ENG FWD COWL SUPPORT RING IS WORN AT THE 9 O'CLOCK POS LOC ON FUSELAGE. REMOVED DAMAGED AREA. FABRICATED DOUBLER AND FILLER PER M/M 53-11-0 PG 801. OK TO INSTALL. INSTALLED REPAIR PER M/M 53-11-0 PG 801.
- [SDR DL72S981764](https://openairdocs.org/sdr/DL72S981764.md): Battery Pack · discharged · Aug 24, 1998 · N407DA · Boeing 727232 · Emergency Lighting
  > ON L/O, AFT OVERWING ESCAPE LIGHT INOP. REPLACED BATTERY PACK.
- [SDR DL72S971562](https://openairdocs.org/sdr/DL72S971562.md): Control Mech · malfunctioned · Aug 8, 1997 · N407DA · Boeing 727232 · Trailing Edge Flap Control System
  > ON APPROACH OUTBD FLAPS WOULD NOT EXTEND. MADE MISSED APPROACH. FLAPS EXTENDED NORMAL ON SECOND ATTEMP. FLAP OPERATIONAL TEST NORMAL ON GROUND AND VISUALLY INSPECTED NO DEFECT FOUND.
- [SDR DL72S970745](https://openairdocs.org/sdr/DL72S970745.md): Sequence Valve · damaged · Apr 22, 1997 · N407DA · Boeing 727232 · Landing Gear Door Retract Section
  > AFTER T/O DURING GEAR RETRACTION, SYS-A PRESSURE/QUANTITY WENT TO 0, A-SYSTEM PUMPS TURNED OFF 1 MIN LATER. CASTING DAMAGED ON LT GEAR DOOR SEQUENCE VALVE. REPLACED SAME.
- [SDR DL72S970292](https://openairdocs.org/sdr/DL72S970292.md): Skin · corroded · Feb 12, 1997 · N407DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > CORROSION REMOVED AROUND RADIO ALTIMETER ANTENNA CUTOUT BTWN FS 520 TO 540, STR 28L AND 29R. INTERNAL REPAIR WILL BE INSTALLED. ADDITIONAL DAMAGE WAS FOUND AT LETTER CHECK ON 041297. CUT OUT 2 IN BY 2.625 IN AT FS 540, STR 28L. A SEPARATE REPAIR WAS INSTAL
- [SDR DL72S962654](https://openairdocs.org/sdr/DL72S962654.md): Power Supply · inoperative · Dec 6, 1996 · N407DA · Boeing 727232 · Emergency Lighting
  > LEFT AFT OVERWING EMERGENCY LIGHT INOP. REPLACED POWER SUPPLY, OPS CHECKS GOOD.
- [SDR DL72S962437](https://openairdocs.org/sdr/DL72S962437.md): Bracket · cracked · Nov 2, 1996 · N407DA · Boeing 727232 · Leading Edge Slat Actuator
  > FOUND ON F1 LETTER CK, NR 1 SLAT ACTUATOR ATTACH BRACKETS CRACKED INBD AND OUTBD SIDES. REPAIRED PER MM 57-20-21.
- [SDR DL72S961425](https://openairdocs.org/sdr/DL72S961425.md): Swivel · leaking · Jun 12, 1996 · N407DA · Boeing 727232 · Hydraulic System, Main
  > DURING CLIMB, A-HYD QTY WENT TO ZERO AND A PUMP LIGHT FLICKERED, RETURNED TO SHV. REPLACED CASE DRAIN FILTERS, NO METAL FOUND. FOUND THE NR 4 SLAT ACTUATOR SWIVEL LEAKING. REPLACED O-RING, REFILLED HYD SYS, RAN ENGINES AND B-PUMPS, OPERATED ALL FLT CONTROLS
- [SDR DL72S961145](https://openairdocs.org/sdr/DL72S961145.md): Bulkhead Web · cracked · Apr 12, 1996 · N407DA · Boeing 727232 · Fuselage Main, Bulkhead
  > THE BS 1183 BULKHEAD WEB WAS FOUND CRACKED AT RBL 26. THERE IS A 1 INCH CRACK AT WL 170. THE WEB IS A BONDED ASSEMBLY OF 2024-T3 CLAD WITH A LOCAL THICKNESS OF 0.050 INCH. THE CRACK LOCATION IS OUTSIDE OF THE INSPECITON AREA SPECIFIED BY BOEING SERVICE BULL
- [SDR DL72S960876](https://openairdocs.org/sdr/DL72S960876.md): Skin · corrosion · Apr 12, 1996 · N407DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > CORROSION DAMAGE WAS REMOVED FROM AROUND THE HOLE CUTOUT FOR THE RADIO ALTIMETER ANTENNA BETWEEN STATION 520 AND STATION 540, BETWEEN STRINGER 28 LEFT AND STRINGER 29 RIGHT. THE SKIN IS MACHINED CLAD 2024-T3 SHEET WITH A LOCAL THICKNESS OF 0.090 THICK. AN IN
- [SDR DL72S960875](https://openairdocs.org/sdr/DL72S960875.md): Skin · corrosion · Apr 12, 1996 · N407DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > CORROSION WAS REMOVED AT STR 28R BETWEEN BS 500 AND BS 520, RESULTING IN A 5.5 BY 2.25 CUT OUT. THERE IS AN EXISTING STRINGER SPLICE AT BS 490 AND A NEW SPLICE BEING INSTALLED AT BS 510 PER B727 SRM. THE SKIN IS MANUFACTURED FROM MACHINED CLAD 2024-T3 WITH A
- [SDR DL72S960843](https://openairdocs.org/sdr/DL72S960843.md): Angle · cracked · Apr 11, 1996 · N407DA · Boeing 727232 · Fuselage Miscellaneous Structure
  > FOUND ON E-2 LETTER CHECK, LWR T-ANGLE CRACKED AT AFT HINGE FOR LWR FUS PANEL 3448R. REPAIRED PER M/M 53-30-1 PG 807.
- [SDR DL72S960512](https://openairdocs.org/sdr/DL72S960512.md): Light · loose · Mar 4, 1996 · N407DA · Boeing 727232 · Emergency Lighting
  > ON PRE-FLIGHT, FOUND SECTION OF TRACK LIGHTING LOOSE WITH EXPOSED WIRING. REPAIRED WIRING SECURED TRACK, OPERATION NORMAL.
- [SDR DL72S960291](https://openairdocs.org/sdr/DL72S960291.md): Sensor · dirty · Feb 6, 1996 · N407DA · Boeing 727232 · Landing Gear Position and Warning
  > ON GEAR RETRACTION, RED RT GEAR AND GREEN RT GEAR LIGHTS REMAINED ON. COMPLETED LDG GEAR RETRACTION MALFUNCTION CHECK LIST, BOTH LIGHTS REMAINED ON. ABOUT 40 SECONDS LATER, BOTH LIGHTS OUT. CHECKED AND CLEANED RIGHT MAIN LANDING GEAR DOWNLOCK, SENSOR OPERAT
- [SDR DL72S960024](https://openairdocs.org/sdr/DL72S960024.md): Skin · cracked · Dec 28, 1995 · N407DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > A SKIN CRACK, 1.75 INCH BY 2 INCH WAS DISCOVERED BETWEEN STRINGER 27R AND 28R, FS 481. THE PREVIOUS REPAIR ON THIS SECTION MEASURED 5.5 INCH BY 13 INCH. THE REPAIRS WERE INCORPORATED INTO ONE REPAIR AFTER REMOVAL OF PREVIOUS REPAIR. THIS ER/A SUPERCEDES ER/
- [SDR DL72S954791](https://openairdocs.org/sdr/DL72S954791.md): Stringer · cracked · Dec 20, 1995 · N407DA · Boeing 727232 · Fuselage Main, Longeron/Stringer
  > FORWARD LOWER FUSELAGE BS-480 STRINGER 28R SKIN BULGING AND CRACKED. REPAIRED PER DL ERA 302938-14.
- [SDR DL72S954747](https://openairdocs.org/sdr/DL72S954747.md): Battery Pack · discharged · Dec 19, 1995 · N407DA · Boeing 727232 · Emergency Lighting
  > EMERGENCY LIGHT OUT LOWER RT OVERWING FAIRING. REPLACED EMERGENCY LIGHT BATTERY PACK. CKS NORMAL.
- [SDR DL72S954709](https://openairdocs.org/sdr/DL72S954709.md): Cooling Valve · failed · Dec 15, 1995 · N407DA · Boeing 727232 · Cabin Cooling System
  > DURING CLIMB AND LEVEL AT FL 240, WERE UNABLE TO MAINTAIN, CABIN SLOWEST RATE OF ASSENT WAS 700 FPM. DESCENDED AND RETURNED TO JFK. FOUND EQUIPMENT COOLING VALVE STUCK OPEN. REPLACED VALVE. RETURNED TO SERVICE.

Next page: https://openairdocs.org/deregistered/N407DA-2001-01-31/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 = 'N407DA' AND deregistration_id = 'N407DA-2001-01-31'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N407DA-2001-01-31/reports

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