# Service difficulty reports: N925L, cancelled Oct 19, 2005

A list on [N925L, cancelled Oct 19, 2005](https://openairdocs.org/deregistered/N925L-2005-10-19.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 · 121 reports

- [SDR TWAA0018301](https://openairdocs.org/sdr/TWAA0018301.md): Socket · cracked · Nov 22, 2000 · N925L · Doug DC932 · Passenger Compartment Lighting
  > AIRCRAFT RETURNED FROM TAXI DUE TO ELECTRICAL SMELL IN AREA OF CABIN ROW 20 AND 21, LEFT SIDE. REPLACED BURNED LIGHT BULB SOCKET AT ROW 20ABC FOR LOWER SIDEWALL LIGHTS. CHECK-C 3-29-00 MCI.
- [SDR TWAA0010401](https://openairdocs.org/sdr/TWAA0010401.md): Bulb · failed · Jul 3, 2000 · N925L · Doug DC932 · Emergency Lighting
  > THE EMERGENCY LIGHT ABOVE THE AFT FLIGHT ATTENDANT SEAT WAS INOPERATIVE. REPLACED THE BULB. CHECK-C 3-29-00 MCI. ---CLOSED---
- [SDR TWAA0004903](https://openairdocs.org/sdr/TWAA0004903.md): Floor Support · cracked · Mar 22, 2000 · N925L · Doug DC932 · Fuselage Miscellaneous Structure
  > DURING OP 16 MAINT CHECK, THE SUPPORT RIBS FOR FLOOR PANEL NUMBER 40 WERE CRACKED. MADE NEW PANEL PER STA SSRM 53-00-104 PAGE 201.
- [SDR TWAA0004302](https://openairdocs.org/sdr/TWAA0004302.md): Frame · cracked · Mar 14, 2000 · N925L · Doug DC932 · Entrance Stairs
  > DURING OP 16 MAINT CHECK, THE VENTRAL STAIRWAY DOOR, LT FRAME O/B OF THE INNER DOOR HANDLE BAR HAD AN 11 INCH CRACK IN THE RADIUS. REMOVED CRACKED FRAME AND FABRICATED NEW FRAME PER DRAWING 9915565.
- [SDR TWAA0003812](https://openairdocs.org/sdr/TWAA0003812.md): Bracket · cracked · Mar 1, 2000 · N925L · Doug DC932 · Wing Miscellaneous Structure
  > DURING OP 16 MAINT CHECK, ON LT WING THE INBD BUTE DOOR ATTACH BRACKET AND REPAIR DOUBLER WERE CRACKED AT AFT END, APPROX 21 INCHES INBD OF INBD FLAP HINGE CASTING. FABRICATED NEW DOUBLER 0.032 SS 301 HALF HARD AND INSTALLED PER SRM 57-01 PAGE 8.
- [SDR TWAA0003202](https://openairdocs.org/sdr/TWAA0003202.md): Flange · cracked · Feb 22, 2000 · N925L · Doug DC932 · Fuselage Miscellaneous Structure
  > DURING OP 16 MAINT CHECK, FOUND IN LT WHEEL WELL THE UPPER FLANGE OF THE TRAPEZONDAL PANEL HAD A CRACK BETWEEN NUMBER 6 AND 9 BOLT HOLES. COMPLIED WITH SERVICE BULETIN 53-182 PER ELMR 70145A.
- [SDR TWAA0003201](https://openairdocs.org/sdr/TWAA0003201.md): Flange · cracked · Feb 22, 2000 · N925L · Doug DC932 · Fuselage Miscellaneous Structure
  > DURING OP 16 MAINT CHECK, IN RT WHEEL WELL FOUND UPPER FLANGE OF TRAPEZONDAL PANEL HAD A CRACK BETWEEN NUMBER 7 AND 8 HOLES. COMPLIED WITH SERVICE BULLETIN 53-182 PER EMLR 70245A.
- [SDR TWAA0003014](https://openairdocs.org/sdr/TWAA0003014.md): Spar · cracked · Feb 15, 2000 · N925L · Doug DC932 · Wing Spar
  > DURING OP 16 MAINT CHECK, RT WING HAD APPROX.375 IN CRACK AT LOWER INBD HOLE ON SURFACE OF REAR SPAR AT INBD FLAP HINGE, STA XRS 164. STOP DRILLED CRACKS PER DAC DRAWING JO 60271. HIGH FREQ EDDY CURRENT ACCOMP PER 51-00-13, PART 6. REPAIRED CRACKED WING SP
- [SDR TWAA0003013](https://openairdocs.org/sdr/TWAA0003013.md): Structure · damaged · Feb 14, 2000 · N925L · Doug DC932 · Fuselage Main, Structure
  > DURING OP 16 MAINT CHECK, NECESSARY TO REPAIR HOLE DAMAGE IN FUSELAGE AT APPORX STA 608 TO 612, LONGERON 28L TO 28R. COMPLIED WITH ARA 16532.
- [SDR TWAA0003012](https://openairdocs.org/sdr/TWAA0003012.md): Skin · corroded · Feb 14, 2000 · N925L · Doug DC932 · Fuselage Main, Plate/Skin
  > DURING OP 16 MAINT CHECK, LOWER FUSELAGE EXISTING REPAIR HAD CORROSION ON FUSELAGE SKIN AFT OF STA 604. REMOVED VISIBLE SURFACE CORROSION PER TWA STD PROCESSES 6-80-01. COMPLIED WITH ARA 16532..
- [SDR TWAA0005810](https://openairdocs.org/sdr/TWAA0005810.md): Angle · cracked · Feb 11, 2000 · N925L · Doug DC932 · Trailing Edge Flaps
  > DURING OP 16 MAINT CHECK, THE LT WING FLAP WAS CRACKED IN UPPER SUPPORT ANGLE ON I/B SIDE OF O/B FLAP HINGE CASTING IN FLANGE. CRACKED ANGLE (P/N 9957600-7) WAS REMOVED AND REPLACED WITH NEW ANGLE PER SPM 6-70-01, PARA 4, SUBSECTION B SRM 51-6--0.
- [SDR TWAA0003011](https://openairdocs.org/sdr/TWAA0003011.md): Longeron · cracked · Feb 11, 2000 · N925L · Doug DC932 · Fuselage Main, Longeron/Stringer
  > DURING OP 16 MAINT CHECK, FUSELAGE STA 579 TO 604 AREA HAD A CRACK IN LONGERON 24L. REPLACED LONGERON 24L PER DAC PRINT 5910068.
- [SDR TWAA0002708](https://openairdocs.org/sdr/TWAA0002708.md): Longeron · broken · Feb 11, 2000 · N925L · Doug DC932 · Fuselage Main, Longeron/Stringer
  > DURING OP 16 MAINT CHECK, LONGERON 25 LT& RT, LONGERON 29 LT STA 579 TO 604 WAS BROKEN OFF AT THE FWD END. REPLACED LONGERON AT EACH AREA AND INSTALLED PER PRINT 5910068.
- [SDR TWAA0002707](https://openairdocs.org/sdr/TWAA0002707.md): Skin · corroded · Feb 10, 2000 · N925L · Doug DC932 · Fuselage Main, Plate/Skin
  > DURING OP 16 MAINT CHECK, THE LOWER FUSELAGE HAD CORROSION COMING FROM MATING SURFACE OF FUSELAGE SKIN AND LONGERONS AT STA 604 TO 617, AND STRINGER 28L TO 29R. REPLACED FUSELAGE SKIN. INSTALLED SKIN PER DRAWING 5911418.
- [SDR TWAA0002613](https://openairdocs.org/sdr/TWAA0002613.md): Longeron · cracked · Feb 9, 2000 · N925L · Doug DC932 · Fuselage Main, Longeron/Stringer
  > DURING OP 16 MAINT CHECK, THE LOWER FUSELAGE, LONGERON 27L, AT STA 566 TO 585, WAS FOUND CRACKED AT THE FWD END. REPLACED CRACKED FITTING WITH (P/N 3920595-501). INSTALLED PER DRAWING 590068.
- [SDR TWAA0002612](https://openairdocs.org/sdr/TWAA0002612.md): Casting · cracked · Feb 9, 2000 · N925L · Doug DC932 · Trailing Edge Flaps
  > DURING OP 16 MAINT CHECK, THE RT WING TRAILING EDGE FLAP O/B HINGE CASTING ATTACH FRAME WAS CRACKED AT I/B AND O/B SIDES. REPLACED CRACKED FRAME PER SRM 51-10-01, PARAGRAPH C.
- [SDR TWAA0002611](https://openairdocs.org/sdr/TWAA0002611.md): Skin · damaged · Feb 9, 2000 · N925L · Doug DC932 · Fuselage Main, Plate/Skin
  > DURING OP 16 MAINT CHECK, FOUND STATIC BURN ON FUSELAGE SKIN AT STA 294, BETWEEN LONGERON 18L AND 19L. NO CRACK PER NDT HFEC PER 51-00-03 PART 6. BLENDED STATIC BURN AND REMOVED RIVET PER SRM 53-04 TABLE A PAGE 208. REPLACED RIVET PER SPM 6-70-01 PAGE 3 AND
- [SDR TWAA0002610](https://openairdocs.org/sdr/TWAA0002610.md): Skin · damaged · Feb 9, 2000 · N925L · Doug DC932 · Fuselage Main, Plate/Skin
  > DURING OP 16 MAINT CHECK, FOUND STATIC BURN ON FUSELAGE SKIN AT STA 164, LONGERON 25L. NO CRACK PER PART 6, 51-00-03. REPLACED RIVET PER SPM 6-70-01 PAGE 3, AND SRM 51-30 AND 51-10-4.
- [SDR TWAA0002609](https://openairdocs.org/sdr/TWAA0002609.md): Rivet · damaged · Feb 9, 2000 · N925L · Doug DC932 · Fuselage Miscellaneous Structure
  > DURING OP 16 MAINT CHECK, ON RT FWD FUSELAGE FOUND RIVET BURN AT APPROX STA 446, 3.5 IN BELOW LONGERON 18R. NO CRACK PER PART 6, 51-00-03. REPLACED RIVET PER SPM 6-70-01 AND SRM 51-30 AND 51-10-4.
- [SDR TWAA0002608](https://openairdocs.org/sdr/TWAA0002608.md): Rivet · damaged · Feb 9, 2000 · N925L · Doug DC932 · Fuselage Miscellaneous Structure
  > DURING OP 16 MAINT CHECK, THE RT FWD FUSELAGE APPROX STA 469 HAD A RIVET BURN 2.75 IN BELOW LONGERON 18R. REPLACED RIVET PER SPM 6-70-01, PAGE 3, SRM 51-30 AND 51-10-4. NO CRACKS PER NDT HIGH FREQ EDDY CURRENT PER 51-00-03, PART 6.
- [SDR TWAA0002406](https://openairdocs.org/sdr/TWAA0002406.md): Channel · damaged · Feb 4, 2000 · N925L · Doug DC932 · Fuselage Miscellaneous Structure
  > DURING OP 16 MAINT CHECK FOUND CABIN AFT VAULT DOOR, WITH TORN METAL U CHANNEL BY RT SIDE OF DOOR JAMB. REPAIRED PER ARA 16326 AND INSTALLED.
- [SDR TWAA0002405](https://openairdocs.org/sdr/TWAA0002405.md): Angle · cracked · Feb 4, 2000 · N925L · Doug DC932 · Fuselage Miscellaneous Structure
  > DURING OP 16 MAINT CHECK FOUND CABIN AFT PRESSURE BULKHEAD DOOR INTERNAL CENTER SUPPORT, FWD T ANGLE CRACKED LT END. REMOVED OLD T ANGLE, MADE NEW ONE AND INSTALLED PER PRINT 9915565.
- [SDR TWAA0002404](https://openairdocs.org/sdr/TWAA0002404.md): Support · cracked · Feb 4, 2000 · N925L · Doug DC932 · Fuselage Miscellaneous Structure
  > DURING OP 16 MAINT CHECK FOUND AFT CABIN PRESSURE BULKHEAD DOOR INTERNAL CENTER SUPPORT WEB CRACKED, LT END WITH END SECTION MISSING. INSTALLED NEW SUPPORT WEB PER PRINT 9915565.
- [SDR TWAA0002403](https://openairdocs.org/sdr/TWAA0002403.md): Casting · cracked · Feb 4, 2000 · N925L · Doug DC932 · Fuselage Miscellaneous Structure
  > DURING OP 16 MAINT CHECK FOUND AFT CABIN PRESSURE BULKHEAD DOOR INTERNAL LT LOWER TOP CASTING CRACKED AT LOWER LEG. REPLACED WITH NEW CASTING PER SERVICE REWORK DRAWING JO60229.
- [SDR TWAA0002402](https://openairdocs.org/sdr/TWAA0002402.md): Fastener · loose · Feb 3, 2000 · N925L · Doug DC932 · Nacelle/Pylon, Plate/Skin
  > DURING OP 16 MAINT CHECK FOUND NUMBER 1 PYLON TOP AFT SKIN HAD 4 ROWS OF BLIND FASTENERS LOOSE AND WORKING. REPLACED UPPER SKIN AND FASTENERS PER DAC DRAWING 9957742, 9915500, 9915501, 9915502, AND 9915503.
- [SDR TWAA0002316](https://openairdocs.org/sdr/TWAA0002316.md): Fastener · misinstalled · Feb 3, 2000 · N925L · Doug DC932 · Nacelle/Pylon, Plate/Skin
  > DURING OP 16 MAINT CHECK ON NUMBER 2 PYLON, TOP OF PYLON SKIN INBD OF AFT ENGINE MOUNT HAD ROW OF SCREWS WITH SKIN WASHERS LOOSE AND IMPROPERLY INSTALLED. REPLACED UPPER SKIN AND FASTENERS PER DAC DRAWING 9957742, 9915500, 9915501, 9915502 AND 9915503.
- [SDR TWAA0002315](https://openairdocs.org/sdr/TWAA0002315.md): Structure · corroded · Feb 2, 2000 · N925L · Doug DC932 · Nacelle/Pylon Structure
  > DURING OP 16 MAINTENANCE CHECK, ON NUMBER 1 PYLON TOP AND BOTTOM OF PYLON FOR ENG MOUNT YOKE STRUCTURE HAD RUSTY SURFACES AT LE ATTACH. CHECKED MATERIAL THICKNESS PER SPM 04-00. REPAIRED PER ARA 16530 AND SRM 54-04 PAGE 77. SHOT PEENED PER DRS 4999.
- [SDR TWAA0002313](https://openairdocs.org/sdr/TWAA0002313.md): Skin · damaged · Feb 2, 2000 · N925L · Doug DC932 · Fuselage Main, Plate/Skin
  > DURING OP 16 MAINTENANCE, CHECK NECESSARY TO INSTALL UPPER WINDOW BELT STRIP FROM STA 699 TO 756 ON LT SIDE. REINSTALLED WINDOW BELT DOUBLER PER MO 71K21 AND EMLR 70533 A.
- [SDR TWAA0002013](https://openairdocs.org/sdr/TWAA0002013.md): Finger Doubler · corroded · Jan 31, 2000 · N925L · Doug DC932 · Fuselage Miscellaneous Structure
  > DURING OP 16 MAINT CHECK, FOUND FUSELAGE CORROSION ON THE LOWER PRESSURE BULKHEAD FINGER DOUBLERS FROM LONGERON 24L TO L24R, STA 604. REPLACED WITH NEW FINGER DOUBLER PER DOUGLAS DRAWING 5914865.
- [SDR TWAA0002012](https://openairdocs.org/sdr/TWAA0002012.md): Tee · damaged · Jan 31, 2000 · N925L · Doug DC932 · Fuselage Miscellaneous Structure
  > DURING OP 16 MAINT CHECK, THE LOWER FUSELAGE LOWER BULKHEAD TEE AT STA 604 REQUIRED REPLACEMENT. CLEANED LOWER BULKHEAD TEE AREA STA 604. REPLACED WITH NEW TEE CORD PER DRAWING 5914865.
- [SDR TWAA0002011](https://openairdocs.org/sdr/TWAA0002011.md): Rib · cracked · Jan 31, 2000 · N925L · Doug DC932 · Nacelle/Pylon, Longeron/Stringer
  > DURING OP 16 MAINT CHECK THE NUMBER 2 ENG PYLON, OTBD SUPPORT RIB WAS CRACKED AT THE FWD END. REPLACED PART PER DAC INSTALLATION PRINT 9915502 AND INSTALLED RIB PN 9915501-502.
- [SDR TWAA0002010](https://openairdocs.org/sdr/TWAA0002010.md): Web · cracked · Jan 31, 2000 · N925L · Doug DC932 · Nacelle/Pylon, Main Frame
  > DURING OP 16 MAINT CHECK, NR 2 PYLON HAD A CRACK IN THE WEB 9.5 INCHES OTBD OF THE FUSELAGE SKIN, TOP OF PYLON AT STA 1038. REPLACED PART PER DAC PRINT INSTALLATION 9915501, INSTALLED RIB 9915501-2.
- [SDR TWAA0002009](https://openairdocs.org/sdr/TWAA0002009.md): Rib · cracked · Jan 31, 2000 · N925L · Doug DC932 · Nacelle/Pylon, Longeron/Stringer
  > DURING OP 16 MAINT CHECK, FOUND NR 2 ENGINE PYLON, INBD RIB WAS CRACKED AT THE FWD END. REPLACED PART PER DAC INSTALLATION PRINT 9915503 AND INSTALLED RIB 9915503-502.
- [SDR TWAA0002008](https://openairdocs.org/sdr/TWAA0002008.md): Keel Beam · corroded · Jan 26, 2000 · N925L · Doug DC932 · Fuselage Main, Keel
  > DURING OP 16 MAINT CHECK, FOUND FUSELAGE STA 607 TO 667 HAD CORROSION ON THE KEEL BEAM. REMOVED CORROSION PER SRM 6-80-01, PAGE 1.
- [SDR TWAA0002312](https://openairdocs.org/sdr/TWAA0002312.md): Fastener · wrong part · Jan 25, 2000 · N925L · Doug DC932 · Fuselage Main, Longeron/Stringer
  > DURING OP 16 MAINTENANCE CHECK, FOUND SEVERAL CHERRY FASTENERS IN UPSIDE DOWN HAT SECTION FROM STA 606 TO 659 AND BETWEEN KEEL AND STRINGER 29R. RE-INSTALLED MS20470AD6 RIVETS PER DRAWING 5911418. INSTALLED RIVETS PER SRM 51-30-2. SUBSTITUTED HL326-6 FOR NA
- [SDR TWAA0002007](https://openairdocs.org/sdr/TWAA0002007.md): Panel · cracked · Jan 21, 2000 · N925L · Doug DC932 · Fuselage Miscellaneous Structure
  > DURING OP 16 MAINT CHECK, FOUND LT MLG WHEEL WELL LT TRAP PANEL AREA, A CRACK HAD MIGRATED BEYOND STOP DRILL AND WAS IN MOUNT BOLT HOLE. CONFIRMED BY HIGH FREQ EDDY CURRENT. REMOVED 718 CASTING AND INSTALLED NEW LT 718 PER SERVICE BULLETIN 53-131 AND SPM 6-7
- [SDR TWAA0001406](https://openairdocs.org/sdr/TWAA0001406.md): Floor Panel · corroded · Jan 19, 2000 · N925L · Doug DC932 · Fuselage Floor Panel
  > DURING OP 16 MAINT CHECK, FOUND CABIN FLOOR PANEL 23 HAD CORROSION. FABRICATED NEW FLOOR PANEL PER SRRM 53-00-104, PAGE 201.
- [SDR TWAA0001414](https://openairdocs.org/sdr/TWAA0001414.md): Support · cracked · Jan 18, 2000 · N925L · Doug DC932 · Fuselage Miscellaneous Structure
  > DURING OP 16 MAINT CHECK, FOUND CABIN FLOOR PANEL NUMBER 26, HAD SUPPORT RIB CRACKED. FABRICATED PANEL PER SSRM 53-00-104, PAGE 102.
- [SDR TWAA0001413](https://openairdocs.org/sdr/TWAA0001413.md): Floor Panel · corroded · Jan 17, 2000 · N925L · Doug DC932 · Fuselage Floor Panel
  > DURING OP 16 MAINT CHECK, FOUND CABIN FLOOR PANEL MEMBER NUMBER 12 HAD CORROSION ON IT. REF CPCP TASK C46-53306 FWD GALLEY AREA. REMOVED CORROSION PER SPM 51-10-3 AND TREATED.
- [SDR TWAA0001412](https://openairdocs.org/sdr/TWAA0001412.md): Support · cracked · Jan 14, 2000 · N925L · Doug DC932 · Fuselage Miscellaneous Structure
  > DURING OP 16 MAINT CHECK, FOUND CABIN FLOOR PANEL 25 SUPPORT RIBS CRACKED. FABRICATED NEW FLOOR PANEL WITH NEW RIBS PER SPM 6-70-01, PAGES 2 AND 3, AND SSRM 53-00-102 PAGE 201.
- [SDR TWAA0001411](https://openairdocs.org/sdr/TWAA0001411.md): Floor Panel · corroded · Jan 14, 2000 · N925L · Doug DC932 · Fuselage Floor Panel
  > DURING OP 16 MAINT CHECK, FOUND CABIN FLOOR PANEL 35 HAD CORROSION. FABRICATED NEW FLOOR PANEL PER SSRM 53-00-104, PAGE 201.
- [SDR TWAA0001410](https://openairdocs.org/sdr/TWAA0001410.md): Support · damaged · Jan 14, 2000 · N925L · Doug DC932 · Fuselage Miscellaneous Structure
  > DURING OP 16 MAINT CHECK, FOUND CABIN FLOOR PANEL 40C SUPPORT RIBS DAMAGED. FABRICATED NEW PANEL PER SSRM 53-00-104, PAGE 201.
- [SDR TWAA0001409](https://openairdocs.org/sdr/TWAA0001409.md): Floor Panel · cracked · Jan 14, 2000 · N925L · Doug DC932 · Fuselage Floor Panel
  > DURING OP 16 MAINT CHECK, FOUND CABIN FLOOR PANEL SCREW HOLES CRACKED IN SEVERAL PLACES, PANEL 48. FABRICATED NEW PANEL PER SSRM 53-00-104, PAGE 201.
- [SDR TWAA0001408](https://openairdocs.org/sdr/TWAA0001408.md): Floor Panel · damaged · Jan 14, 2000 · N925L · Doug DC932 · Fuselage Floor Panel
  > DURING OP 16 MAINT CHECK, FOUND CABIN FLOOR PANEL 77, HAD THE END OF THE PANEL BROKEN OUT. FABRICATED NEW PANEL PER SSRM 53-00-104, PAGE 201.
- [SDR TWAA0001407](https://openairdocs.org/sdr/TWAA0001407.md): Floor Panel · damaged · Jan 14, 2000 · N925L · Doug DC932 · Fuselage Floor Panel
  > DURING OP 16 MAINT CHECK, FOUND CABIN FLOOR PANEL 42 HAD BOTTOMSIDE IN CHANNEL. FABRICATED NEW PANEL PER SSRM 53-00-104, PAGE 201..
- [SDR TWAA0001405](https://openairdocs.org/sdr/TWAA0001405.md): Support · cracked · Jan 14, 2000 · N925L · Doug DC932 · Fuselage Miscellaneous Structure
  > DURING OP 16 MAINT CHECK, FOUND FLOOR PANEL 40A SUPPORT RIBS CRACKED. REPLACED SUPPORT RIBS WHILE FABRICATING NEW FLOOR PANEL PER SSRM 53-00-104, PAGE 201. PICKED UP HOLES ON PANEL 40A.
- [SDR TWAA0001009](https://openairdocs.org/sdr/TWAA0001009.md): Floor Panel · damaged · Jan 7, 2000 · N925L · Doug DC932 · Fuselage Floor Panel
  > DURING OP 16 MAINT CHECK, FOUND CABIN FLOOR PANEL NUMBER 40B WITH FIELD REPAIR. MADE NEW FLOOR PANEL PER TWA SSRM 53-00-104, PAGE 201.
- [SDR TWAA0001008](https://openairdocs.org/sdr/TWAA0001008.md): Floor Panel · corroded · Jan 6, 2000 · N925L · Doug DC932 · Fuselage Floor Panel
  > DURING OP 16 MAINT CHECK, PANEL NUMBER 44 HAD GOUGES AT END OF TOP HATS AND CORROSION AT OPPOSITE END. FABRICATED NEW FLOOR PANEL PER SSRM 53-00-104, PAGE 201.
- [SDR TWAA0001007](https://openairdocs.org/sdr/TWAA0001007.md): Floor Panel · broken · Jan 6, 2000 · N925L · Doug DC932 · Fuselage Floor Panel
  > DURING OP 16 MAINT CHECK, NUMBER 21 FLOOR PANEL CORNER WAS BROKEN. FABRICATED NEW PANEL PER SSRM 53-00-14, PAGE 201.
- [SDR TWAA0001006](https://openairdocs.org/sdr/TWAA0001006.md): Floor Panel · cracked · Jan 6, 2000 · N925L · Doug DC932 · Fuselage Floor Panel
  > DURING OP 16 MAINT CHECK, FOUND FLOOR PANEL 19 SUPPORT RIBS WERE CRACKED. FABRICATED NEW FLOOR PANEL PER SSRM 53-00-104, PAGE 201..

Next page: https://openairdocs.org/deregistered/N925L-2005-10-19/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 = 'N925L' AND deregistration_id = 'N925L-2005-10-19'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N925L-2005-10-19/reports

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