# Service difficulty reports: N920DE, cancelled Nov 29, 2022

A list on [N920DE, cancelled Nov 29, 2022](https://openairdocs.org/deregistered/N920DE-2022-11-29.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 4 · 178 reports

- [SDR DALA2020012500595](https://openairdocs.org/sdr/DALA2020012500595.md): Line · leaking · Jan 24, 2020 · N920DE · Doug MD88 · Hydraulic System, Main
  > AFTER LANDING & STARTING THE APU & SHUTTING DOWN RIGHT ENGINE WE SMELLED A DIRTY SOCK SMELL WITH SOULE HAZE IN CABIN SHUT DOWN RIGHT PACK & IT DIDN'T GET WORSE BUT DIDN'T GO AWAY. FOUND LEAK COMING FROM RT RUDDER CONTROL PRESSURE LINE. REPLACED LINE C/W NO GO
- [SDR DALA2020011300211](https://openairdocs.org/sdr/DALA2020011300211.md): Unknown · odor · Jan 12, 2020 · N920DE · Doug MD88 · Air Distribution System
  > AT TAKEOFF A STRONG RUBBER TIRE SMELL FILLED THE CABIN NOI VIBRATION OR ANY OTHER INDICATION OF A PROBLEM SMELL WAS STRONG BUT DISSIPATED IN APPX 2 MIN.C/W AMDS CARD 2120-2367 PNEUMATIC DISTRIBUTION T/S. ALO AMDS CARD 7100-2619 PNEUMATIC SYSTEM DUCT BURN APU W
- [SDR DALA2019101215864](https://openairdocs.org/sdr/DALA2019101215864.md): Battery · missing · Oct 10, 2019 · N920DE · Doug MD88 · Smoke Detection
  > LAVATORY SMOKE DETECTOR BATTERY MISSING. REPLACED THE BATTERY, OP CKS NML.
- [SDR DALA2019051403011](https://openairdocs.org/sdr/DALA2019051403011.md): Light · inoperative · May 14, 2019 · N920DE · Doug MD88 · Emergency Lighting
  > EMERGENCY LIGHT OVER DOOR AT 24A INOP. RELAMPED SAME OPS NML REF AMM 33-52. (LP4751576)
- [SDR DALA2019030801553](https://openairdocs.org/sdr/DALA2019030801553.md): Relay · defective · Mar 7, 2019 · N920DE · Doug MD88 · Air Distribution System
  > AFTER TAKE OFF SMELL OF BURNT RUBBER IN COCKPIT AND CABIN. DISSIPATED QUICKLY. GONE BY APPROXIMATELY 10,000 FEET. R/R RECIRC FAN. NO HELP. REPLACED RELAY R2-278. (LP5733780)
- [SDR DALA2019021100875](https://openairdocs.org/sdr/DALA2019021100875.md): Wire Harness · damaged · Feb 11, 2019 · N920DE · Doug MD88 · Light System Wiring
  > EMERGENCY PATH LIGHT INOP @ PX 19&22. R/R SEAT WIRING HARNESS AT PAX 19&22 CKS GOOD PER AMM MD88 33-53. (LP5277974)
- [SDR DALA2018100405888](https://openairdocs.org/sdr/DALA2018100405888.md): Nose Cowl · dented · Oct 3, 2018 · N920DE · Doug MD88 · Engine Cowling System
  > DURING INSP. FOUND DENT ON NR 1 ENG INLET NOSE COWL AT 10 O'CLOCK POSITION. DENT MEASURES 2.25" X 1.25" & 0.344 DEEP & APPROX 10 O'CLOCK POSITION. PEFORMED TIME LIMITED REPAIR PER ERA 572070-14 SECTION I. NO CRACKS NOTED. REPLACED NR 1 ENGINE NOSE COWL PER RI
- [SDR DALA2018050803134](https://openairdocs.org/sdr/DALA2018050803134.md): Battery Pack · discharged · May 4, 2018 · N920DE · Doug MD88 · Emergency Lighting
  > DURING EMERGENCY LIGHT TEST DO NOT TURN ON, EXTERNAL LIGHTS ON FUSELAGE. REPLACED BATTERY PACK P/N60-1177-9IN AFT CARGO. OPS CHECKS OK.
- [SDR DALA201805173006](https://openairdocs.org/sdr/DALA201805173006.md): Slide · malfunctioned · May 2, 2018 · N920DE · Doug MD88 · Escape Slide
  > DURING INITIAL INSPECTION, FOUND THAT THE FIRING LANYARD TO CONNECT MANUAL INFLATION HANDLE WAS MISSING ON THE L2 DOOR SLIDE, THE SAME SLIDE WAS FOUND WRAPPED AROUND WITH A NYLON CORD. L2 DOOR SLIDE WAS REMOVED AND REPLACED IAW AMM 25-62-00.
- [SDR DALA2018050202977](https://openairdocs.org/sdr/DALA2018050202977.md): Frame · worn · May 1, 2018 · N920DE · Doug MD88 · Fuselage Main, Frame
  > WORN FRAME ON STA Y=1510 CANT BTW 4-8 HRS POSITION AT AFT ACCESSORIES COMPARTMENT. FRAME WAS BLENDED OUT PER SRM 53-01 FIG. 1, FRAME BTW 6 AND 8 POSITION FOUND WITHIN LIMITS. FRAME AT 4 HRS POSITION MINIMUM REMAINING THICKNESS IS 0.027" THEREFORE IT IS OUT OF
- [SDR DALA2018050102952](https://openairdocs.org/sdr/DALA2018050102952.md): Spar Cap · cracked · Apr 30, 2018 · N920DE · Doug MD88 · Horizontal Stabilizer, Spar/Rib
  > DUE A CRACK ON RT HORIZONTAL STABILIZER REAR SPAR CAP, REMOVE AND INSTALL RUDDER. RUDDER WAS REMOVED AND INSTALLED UNDER AMDS 2720-4421 JOB 000-0030.
- [SDR DALA2018043002894](https://openairdocs.org/sdr/DALA2018043002894.md): Rib · cracked · Apr 29, 2018 · N920DE · Doug MD88 · Wing, Rib/Bulkhead
  > CRACKED RIB, XRS 214, RT WING LEADING EDGE INNER STRUCTURE. THE RIB WAS REPLACED IAW SRM 51-30-2.
- [SDR DALA2018043002893](https://openairdocs.org/sdr/DALA2018043002893.md): Cusp Web · corroded · Apr 29, 2018 · N920DE · Doug MD88 · Fuselage Miscellaneous Structure
  > CORROSION FOUND ON THE RT CUSP WEB, UPPER & LOWER SURFACES, RBL 54 TO 60 BETWEEN BS 484 TO 503. THE CUSP WEB WAS REPLACED IAW SRM 5130-2, 51-30-1, AND 51-30-5.
- [SDR DALA2018043002892](https://openairdocs.org/sdr/DALA2018043002892.md): Spar Cap · cracked · Apr 29, 2018 · N920DE · Doug MD88 · Horizontal Stabilizer, Spar/Rib
  > CRACK FOUND ON THE RT HORIZONTAL STABILIZER REAR SPAR CAP. THE SPAR CAP WAS REPLACED IAW 5510-4135.
- [SDR DALA2018042902889](https://openairdocs.org/sdr/DALA2018042902889.md): Frame · cracked · Apr 28, 2018 · N920DE · Doug MD88 · Fuselage Main, Frame
  > CRACK FOUND ON THE FRAME AT BS 1474, AT THE 8 HRS POSITION IN THE AFT ACCESORY BAY. THE FRAME WAS REPAIRED IAW ER/A 567630-14, REV ORIGINAL, & ETI-88-18-033, REV ORIGINAL.
- [SDR DALA2018042802885](https://openairdocs.org/sdr/DALA2018042802885.md): Frame · worn · Apr 28, 2018 · N920DE · Doug MD88 · Fuselage Main, Frame
  > FRAME FOUND WORN OUT OF LIMITS, BS 1485, BETWEEN THE 9 AND 10 HRS POSITION. THE FRAME WAS REPAIRED IAW ER/A 567923-14, REV ORIGINAL, AND ETI-88-18-039, REV 2.
- [SDR DALA2018042802882](https://openairdocs.org/sdr/DALA2018042802882.md): Frame · cracked · Apr 27, 2018 · N920DE · Doug MD88 · Fuselage Main, Frame
  > A CRACK WAS FOUND ON THE FRAME WEB BS 1437, LONGERON 8L. REPAIRED IAW ERA 567707-14, REV ORIGINAL, AND ETI-88-18-021, R3.
- [SDR DALA2018042702844](https://openairdocs.org/sdr/DALA2018042702844.md): Pan · corroded · Apr 27, 2018 · N920DE · Doug MD88 · Fuselage Miscellaneous Structure
  > CORROSION FOUND ON THE LOWER PAN, BS 370 TO 427, LONGERONS 23R TO 28R AT THE CARGO DOOR FRAME. THE PAN WAS REPAIRED IAW ETI-88-18-025, REV 1, AND ER/A 567912-14, REV ORIGINAL.
- [SDR DALA2018042702845](https://openairdocs.org/sdr/DALA2018042702845.md): Skin · damaged · Apr 26, 2018 · N920DE · Doug MD88 · Rudder, Plate/Skin
  > FOUND DAMAGED ALUMINUM FLAME SPRAY, LT & RT SIDES, SEVERAL AREAS. ON THE RUDDER. THE FRAME SPRAY WAS REPARIED IAW ERA.092613-14MA, REV C.
- [SDR DALA2018042602825](https://openairdocs.org/sdr/DALA2018042602825.md): Finger Doubler · corroded · Apr 25, 2018 · N920DE · Doug MD88 · Fuselage Main, Plate/Skin
  > CORROSION ON THE FINGER DOUBLER BETWEEN BS 1210 AND 1215, LONGERON 26L. FOUND TO BE OUT OF LIMITS. THE FINGER DOUBLER WAS REPLACED IAW SRM 53-04, FIG 12E, & SRM 51-30-2.
- [SDR DALA2018042502804](https://openairdocs.org/sdr/DALA2018042502804.md): Skin · damaged · Apr 23, 2018 · N920DE · Doug MD88 · Wing Spar
  > CRACKS, PUNCTURES AND WEAR FOUND ON THE FIXED LEADING EDGE SKIN BETWEEN XFS 60 - 70, RT WING. REPAIRED IAW ERA 567673-14, REV B, AND ETI -88-18-031, REV 6.
- [SDR DALA2018042302706](https://openairdocs.org/sdr/DALA2018042302706.md): Floor Panel · corroded · Apr 22, 2018 · N920DE · Doug MD88 · Fuselage Floor Panel
  > CORRODED FLOOR PANEL. THE FLOOR PANEL WAS REPLACED IAW AMM 53-20-01.
- [SDR DALA2018042202697](https://openairdocs.org/sdr/DALA2018042202697.md): Floor Panel · damaged · Apr 21, 2018 · N920DE · Doug MD88 · Fuselage Floor Panel
  > DELAMINATED COMPOSITE MATERIAL, PUNCTURES ON CHANNELS AND CORROSION ON STRAP AT FLOOR PANEL 200A. THE FLOOR PANEL AND CHANNELS WERE REPAIRED IAW SRM 51-70-1D, PAR. 10. AND DWG 9952523, REV Y.
- [SDR DALA2018042202695](https://openairdocs.org/sdr/DALA2018042202695.md): Frame · cracked · Apr 21, 2018 · N920DE · Doug MD88 · Fuselage Main, Frame
  > CRACKED FRAME BS 1474, LONGERON 18R IN THE AFT ACCESORIES BAY. THE FRAME WAS REPAIRED IAW ER/A 567556-14, REV ORIGINAL, & ETI-88-18-023 R1.
- [SDR DALA2018042202694](https://openairdocs.org/sdr/DALA2018042202694.md): Cusp Web · corroded · Apr 21, 2018 · N920DE · Doug MD88 · Fuselage Miscellaneous Structure
  > CORROSION ON CUSP WEB LOWER SURFACE BS 1155 TO 1212, RBL 54 TO 60 IN THE AFT CARGO BAY. REPLACED IAW SRM 53-05, FIG 131A-24, SRM 51-30-2, & 51-30-5.
- [SDR DALA2018042102685](https://openairdocs.org/sdr/DALA2018042102685.md): Shear Tie · cracked · Apr 20, 2018 · N920DE · Doug MD88 · Fuselage Internal Mounting Structure
  > CRACK ON THE SHEAR TIE BS 1380, LONGERON 15R IN THE AFT ACCESORIES COMPARTMENT. THE SHEAR TIE WAS REPLACED IAW SRM 51-30-5, & DWG 9912246, REV CY.
- [SDR DALA2018042002660](https://openairdocs.org/sdr/DALA2018042002660.md): Frame Angle · cracked · Apr 19, 2018 · N920DE · Doug MD88 · Fuselage Main, Frame
  > AFTER REMOVING CORROSION, A CRACK WAS FOUND ON THE CAP ANGLE ATTACHED TO STAIRWAY FRAME, BETWEEN BS 1401 - 1405, LT SIDE. THE CAP ANGLE WAS REPLACED IAW SRM 51-30-2.
- [SDR DALA2018042002657](https://openairdocs.org/sdr/DALA2018042002657.md): Skin · corroded · Apr 19, 2018 · N920DE · Doug MD88 · Fuselage Main, Plate/Skin
  > CORROSION FOUND ON THE FUSELAGE SKIN BETWEEN BS 769 - 776, LONGERONS 27R - 28R. THE SKIN WAS REPAIRED IAW SRM 53-04, FIG 57.
- [SDR DALA2018041802587](https://openairdocs.org/sdr/DALA2018041802587.md): Tee Fitting · corroded · Apr 17, 2018 · N920DE · Doug MD88 · Fuselage Miscellaneous Structure
  > CORROSION ON THE TEE FITTING, BS 1380 BETWEEN LONGERONS 25L & 25R. THE TEE FITTING WAS REPLACED IAW SRM 51-30-2, AND 51-30-5.
- [SDR DALA2018041802586](https://openairdocs.org/sdr/DALA2018041802586.md): Floor Support · damaged · Apr 17, 2018 · N920DE · Doug MD88 · Fuselage Miscellaneous Structure
  > ELONGATED HOLE ON THE FLOOR SUPPORT BS 826, RBL 22. REPAIRED IAW ERA 567554-14, REV ORIG, AND ETI-88-18-022, REV ORIG.
- [SDR DALA2018041702528](https://openairdocs.org/sdr/DALA2018041702528.md): Frame · cracked · Apr 17, 2018 · N920DE · Doug MD88 · Fuselage Main, Frame
  > A CRACK WAS FOUND ON THE FRAME, BS 1510. THE FRAME WAS REPLACED IAW SRM 51-30-1, 51-30-2, AND 51-30-5.
- [SDR DALA2018041702533](https://openairdocs.org/sdr/DALA2018041702533.md): Vane · delaminated · Apr 16, 2018 · N920DE · Doug MD88 · Trailing Edge Flaps
  > DURING INSPECTION, DELAMINATED WAS FOUND ON THE PREVIOUS DOUBLER REPAIR ON OTBD FLAP VANE OF OTBD FLAP, LT WING. THE FLAP VANE WAS REPLACED IAW SRM 57-04, PAR. 5
- [SDR DALA2018041702530](https://openairdocs.org/sdr/DALA2018041702530.md): Tab · dented · Apr 16, 2018 · N920DE · Doug MD88 · Elevator, Tab Structure
  > DURING INSPECTION, FOUND SEVERAL DENTS ON UPPER SKIN AT THE RT CONTROL TAB. THE RT CONTROL TAB WAS REPLACED IAW 55-04 PAR 2.
- [SDR DALA2018041702521](https://openairdocs.org/sdr/DALA2018041702521.md): Fitting · cracked · Apr 16, 2018 · N920DE · Doug MD88 · Fuselage Main, Attach Fittings
  > CRACKED FITTINGS AT THE RT AND LT SIDES AT AFT CABIN BULKHEAD DOOR FRAME. FITTINGS REPLACED IAW SRM 51-30-2, 51-30-5, AND 51-30-1.
- [SDR DALA2018041602514](https://openairdocs.org/sdr/DALA2018041602514.md): Tab · dented · Apr 15, 2018 · N920DE · Doug MD88 · Elevator, Tab Structure
  > SEVERAL DENTS ON UPPER SKIN AT THE LT GEARED TAB. THE TAB WAS REPLACED IAW 55-04, PAR 2.
- [SDR DALA2018041602513](https://openairdocs.org/sdr/DALA2018041602513.md): Tab · debonded · Apr 15, 2018 · N920DE · Doug MD88 · Elevator, Tab Structure
  > DISBONDED UPPER AND LOWER SKIN AT LT ANTI FLOAT TAB, XEFT 160. THE LT ANTI-FLOAT TAB WAS REPLACED IAW 55-04, PAR 2.
- [SDR DALA2018041502435](https://openairdocs.org/sdr/DALA2018041502435.md): Channel · cracked · Apr 14, 2018 · N920DE · Doug MD88 · Fuselage Miscellaneous Structure
  > CRACK CHANNEL ON GENERATION FLOOR NBR 313A, 313E, 389G, 541F, 617G, 927A AND 927E. CHANNEL ON GENERATION FLOOR NBR 313A, 313E, 389G, 541F, 617G AND 927E WERE REPAIR PER DC-9/MD-80 SRM 53-05 FIG.131B AND 131C (SHEET 1), AND FLOOR PANEL NBR. 927A WAS REPLACED P
- [SDR DALA2018041402429](https://openairdocs.org/sdr/DALA2018041402429.md): Access Panel · corroded · Apr 13, 2018 · N920DE · Doug MD88 · Wing, Plate/Skin
  > CORROSION ON RH FUEL ACCESS PLATES NBR 1436C, 1454C, 1414C, 1478C AND 1470C. FUEL ACCES PLATE 1454C, 1436C, 1414C, 1478C AND 1470C WERE REPLACED PER DC9/MD-80 SRM 51-22-2A. (LP0507595)
- [SDR DALA2018041402427](https://openairdocs.org/sdr/DALA2018041402427.md): Access Panel · corroded · Apr 13, 2018 · N920DE · Doug MD88 · Wing, Plate/Skin
  > CORROSION ON LH FUEL ACCESS PLATES NBR 1311C, 1335C AND 1363C. ACCESS PLATE NBR 1311C, 1335C AND 1363C WERE REPLACED PER DC-9/MD-80 SRM 51-22-2A PAR 6 (LP0507458)
- [SDR DALA2018041402432](https://openairdocs.org/sdr/DALA2018041402432.md): Fitting · cracked · Apr 13, 2018 · N920DE · Doug MD88 · Fuselage Miscellaneous Structure
  > CRACK ON SHEAR CLIP STA Y= 1380 LONG 15L AT AFT ACCESSORIES COMPARTMENT. FRAME CLIP WAS REPLACED PER SRM 53-14-4 & DWG 9912246 REV CY.
- [SDR DALA2018041402431](https://openairdocs.org/sdr/DALA2018041402431.md): Floor Panel · damaged · Apr 13, 2018 · N920DE · Doug MD88 · Fuselage Floor Panel
  > ELONGATED HOLES ON COCKPIT FLOOR PANEL NR 120B LT SIDE. FLOOR WAS REPAIRED (PERMANENT REPAIR) PER DC-9/MD-80 SRM 53-01 FIG 4 (SHEET4).
- [SDR DALA2018041402430](https://openairdocs.org/sdr/DALA2018041402430.md): Floor Panel · cracked · Apr 13, 2018 · N920DE · Doug MD88 · Fuselage Floor Panel
  > CRACK COCKPIT RT FLOOR PANEL NR 120D. FLOOR PANEL WAS REPAIRED (PERMANENT REPAIR) PER SRM 53-01 FIG 2 (SHEET3).
- [SDR DALA2018041402428](https://openairdocs.org/sdr/DALA2018041402428.md): Floor Panel · cracked · Apr 13, 2018 · N920DE · Doug MD88 · Fuselage Floor Panel
  > CRACK UPPER SKIN ON GENERATION FLOOR NR 465E AND 826G. FLOOR NR 465E AND 826G WERE REPAIRED (AS A PERMANENT REPAIR) PER SRM 53-01 FIG.2 (SHEET3) AND FIG 4 (SHEET4).
- [SDR DALA2018041302407](https://openairdocs.org/sdr/DALA2018041302407.md): Access Panel · corroded · Apr 12, 2018 · N920DE · Doug MD88 · Wing, Plate/Skin
  > CORROSION ON LH/RH FUEL ACCESS PLATES NBR 1303C AND 1409C IN REF AMDS 2000-2636. DUE TO BLEND OUT REPAIR IS NOT PERMITTED ON THE UPPER WING ACCESS DOOR (P/N 3912757) DUE TO THE REDUCED AREA OF THE CONDUCTIVE INTERFACE. FUEL ACCESS DOOR 1409C AND 1303C WERE REP
- [SDR DALA2018041302406](https://openairdocs.org/sdr/DALA2018041302406.md): Floor Support · cracked · Apr 12, 2018 · N920DE · Doug MD88 · Fuselage Miscellaneous Structure
  > CRACKED FLOOR SUPPORT, BS 1271 TO 1287, LBL 2. REPAIRED IAW SRM 53-01, PAR. 4 FIG.2, SHEET 4.
- [SDR DALA2018041102337](https://openairdocs.org/sdr/DALA2018041102337.md): Floor Panel · cracked · Apr 11, 2018 · N920DE · Doug MD88 · Fuselage Floor Panel
  > INITIAL INSPECTION CRACKS ON FLOOR PANELS NBRS 168B, 200C, 160A, 389F AND 1003B AT PAX CAB. FLOOR PANELS NBRS 168B, 200C, 160A,389F AND 1003B WERE FABRICATED REPLACED AND IDENTIFIED PER MD88 A.M.M. 53-20-01-201 AND WERE INSTALLED PER ROUTINE TASK CARD 001-007
- [SDR DALA2018041102336](https://openairdocs.org/sdr/DALA2018041102336.md): Floor Panel · delaminated · Apr 11, 2018 · N920DE · Doug MD88 · Fuselage Floor Panel
  > INITIAL INSPECTION DELAMINATION ON FLOOR PANELS NBRS 160D, 120C, 160C, 160E, 200D, 200B, 1174E, 160F, 617D, 617E, 617F, 769E, 769F, AND 826E. FLOOR PANELS NBRS 160D, 120C, 160C, 160E, 200D, 200B, 1174E, 160F, 617D, 617E 617F, 769E, 769F, AND 826E WERE FABRICAT
- [SDR DALA2018041202380](https://openairdocs.org/sdr/DALA2018041202380.md): Cusp Web · corroded · Apr 11, 2018 · N920DE · Doug MD88 · Fuselage Miscellaneous Structure
  > CORROSION ON RT CUSP WEB STA Y =1072 AT CPAX. CORROSION 2: REPAIR WAS ACCOMPLISHED (PERMANENT REPAIR) PER SRM53-05 FIG 131-A-13.
- [SDR DALA2018041202378](https://openairdocs.org/sdr/DALA2018041202378.md): Longeron · cracked · Apr 11, 2018 · N920DE · Doug MD88 · Fuselage Main, Longeron/Stringer
  > CRACK LONG 12L STA Y=1437 AT AFT ACCESSORIES COMPARTMENT. LONG 12L STA Y=1437 AT AFT ACCESSORIES WAS REPAIR ( AS A PERMANENT REPAIR)PER SRM 53-02-FIG.18, SRM 51-30-5 AND SRM 51-30-2.
- [SDR DALA2018041202374](https://openairdocs.org/sdr/DALA2018041202374.md): Cusp Web · corroded · Apr 11, 2018 · N920DE · Doug MD88 · Fuselage Miscellaneous Structure
  > CORROSION ON LT CUSP WEB STA X=54 TO X=60 BTW STA Y=674 AND Y=693. CORROSION 2; LT CUSP WEB STA X=54 TO X=60 BTW STA Y=674 AND Y=693 WAS REPAIRED (PERMANENT REPAIR) PER SRM 53-05 FIG 131A-9.

Next page: https://openairdocs.org/deregistered/N920DE-2022-11-29/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 = 'N920DE' AND deregistration_id = 'N920DE-2022-11-29'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N920DE-2022-11-29/reports

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