# Service difficulty reports: N922DL, cancelled Sep 20, 2022

A list on [N922DL, cancelled Sep 20, 2022](https://openairdocs.org/deregistered/N922DL-2022-09-20.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 · 159 reports

- [SDR DALA2019072804443](https://openairdocs.org/sdr/DALA2019072804443.md): Slide · defective · Jul 28, 2019 · N922DL · Doug MD88 · Escape Slide
  > DURING SCHEDULED DEPLOYMENT TEST, SLIDE FAILED TO DEPLOY REF CARD 2562-7193 FORECAST NO 88-0525-8-0407. SLIDE FAILED TO DEPLOY DUE TO FIRING LANYARD NOT BEING INSTALLED THROUGH THE TAB AND ON THE RETAINING RING. INSTALL OF NEW SLIDE PERFORMED ON TASK CARD 2561
- [SDR DALA2019042002531](https://openairdocs.org/sdr/DALA2019042002531.md): Stiffener · cracked · Apr 19, 2019 · N922DL · Doug MD88 · Turbine Engine Air Inlet Section
  > NOSE COWL CRACKED. INTERNAL FWD BULKHEAD STIFFENER AT 07:00 UPPER AND LOWER FAST. HOLES (2 AREAS)MARKED. INTERNAL FWD BULKHEAD STIFFENER AT 6:30 LOWER FAST. EXTERNAL STIFFENER AT 6.30 MARKED. REM/REPL #1 ENG NOSE COWL PER MD88 AMM 71-10. COWL, NOSE, LT OFF 88-
- [SDR DALA2019020600811](https://openairdocs.org/sdr/DALA2019020600811.md): Battery Pack · inoperative · Feb 6, 2019 · N922DL · Doug MD88 · Emergency Lighting
  > OVERHEAD EMERGENCY LIGHTS OUT 22, 23, 24, 25 ROWS. R/R BATTERY SET AT BATTERY PACK B5-104 IAW MD88 AMM 33-53. OPS CK GOOD. (LP5319148)
- [SDR DALA2019011600274](https://openairdocs.org/sdr/DALA2019011600274.md): Outlet · damaged · Jan 10, 2019 · N922DL · Doug MD88 · Passenger Compartment Equipment
  > PAX 4B NOTICED PED CHARGING STATION DAMAGED/CHARRED. NO SMOKE. REPLACED OUTLET, OPS GOOD. (LP5162466)
- [SDR DALA2019010400035](https://openairdocs.org/sdr/DALA2019010400035.md): Pin · pulled · Jan 3, 2019 · N922DL · Doug MD88 · Escape Slide
  > FOUND 1L DOOR SLIDE PIN PULLED OUT. REPLACED 1L DOOR SLIDE ASSY PER W/C 5200-0652. OK FOR SVC. SLIDE, PASSENGE OFF 09-2561-9-0011 00147. (LP5162443)
- [SDR DALA2018121407183](https://openairdocs.org/sdr/DALA2018121407183.md): Frame · cracked · Dec 13, 2018 · N922DL · Doug MD88 · Fuselage Main, Frame
  > CRACK- 1310 CANT FRAME CRACKED AT TAIL CONE GUIDE PIN 4 OCLOCK POSITION. REMOVED DAMAGED FRAME PN 5966769U501. (458779) DRILLED NEW FRAME AND BEGAN INSTALLATION PER BOEING DWG 5966769. COMPLETED INSTALLATION OF FRAME PER BOEING DWG 5966769. (LP0863490)
- [SDR DALA2018072304609](https://openairdocs.org/sdr/DALA2018072304609.md): Bracket · out of adjust · Jul 23, 2018 · N922DL · Doug MD88 · Emergency Lighting
  > EMERGENCY SEAT ISLE LIGHT INOP AT SEAT 31 DE. ADJUSTED BRACKET AND BULB FIXTURE AT ISLE SEAT 31 DE. OPS CK GOOD.
- [SDR DALA2018101005977](https://openairdocs.org/sdr/DALA2018101005977.md): Skin · corroded · May 14, 2018 · N922DL · Doug MD88 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN, STA 750, L-30 CORROSION REPAIR, PERMANENT REPAIR. C/W ERA 455233-14 REV C, MON CLOSED.
- [SDR DALA2018032801981](https://openairdocs.org/sdr/DALA2018032801981.md): Window · out of adjust · Mar 28, 2018 · N922DL · Doug MD88 · Flight Compartment Windows
  > FIRST OFFICER'S EMERGENCY ESCAPE WINDOW WILL NOT OPEN. ADJUSTED THE WINDOW IAW AMM 56-10. OPS CHECKED GOOD.
- [SDR DALA2018032601875](https://openairdocs.org/sdr/DALA2018032601875.md): Nut · loose · Mar 25, 2018 · N922DL · Doug MD88 · Turbine Engine Oil System
  > AT FL330 MASTER CAUTION LOW OIL PRESS RIGHT ENG. RAN QRH, 0 QUANTITY, THEN SHUT DOWN R ENGINE. R PRESSURE AND QUANTITY BOTH 0. WINDMILL 15 MINUTES. UPON ARRIVAL FOUND LOWER COWL COVERED WITH OIL. FOUND LOOSE STUD/NUT ON OIL FILTER CAP W/O-RING PROTRUDING. WIP
- [SDR DALA2018030201318](https://openairdocs.org/sdr/DALA2018030201318.md): Wire Harness · inoperative · Mar 2, 2018 · N922DL · Doug MD88 · Light System Wiring
  > EMERGENCY LIGHT AT SEAT 20 DE INOPERATIVE. REPLACED THE SEAT WIRE HARNESS IAW AMM 33-52. CHECKED GOOD.
- [SDR DALA2017092507058](https://openairdocs.org/sdr/DALA2017092507058.md): Panel · corroded · Sep 24, 2017 · N922DL · Doug MD88 · Airfoil Anti/De-ice System
  > CORROSION ON RT HEATER BLANKET AROUND ACCESS NR 1410C CUT OUT (AD). LEVEL CORROSION 2. RT HEATER BLANKET PANEL WAS REPLACED PER AMM 30-80-02-401 BLOCK 401. OVERWING HEATER BLANKET FUNCTIONAL TEST WAS PERFORMED PER AMM 30-80-02-0501. TEST OK.
- [SDR DALA2017092407057](https://openairdocs.org/sdr/DALA2017092407057.md): Door Frame · damaged · Sep 23, 2017 · N922DL · Doug MD88 · Fuselage Main, Structure
  > AWR HIDDEN DAMAGE: ELONGATED HOLES ON LOWER DOOR JAMB BEAM STA Y=636 TO Y=693 AT MID CARGO COMPARTMENT. ELONGATED HOLES ON LOWER DOOR JAMB BEAM STA Y=636 TO Y=693 AT MID CARGO COMPARTMENT WERE REPAIRED PER ETI-88-17-235 REV 3 AND ER/A 560942-14 REV ORG.
- [SDR DALA2017092207015](https://openairdocs.org/sdr/DALA2017092207015.md): Spacer · corroded · Sep 21, 2017 · N922DL · Doug MD88 · Fuselage Miscellaneous Structure
  > CORROSION ON SPACER AT MID CARGO COMPARTMENT DOOR JAMB BEAM REPAIR ALSO THE REPAIR DOES NOT MEET REQUIREMENTS PER SRM (SM) (C2) (IN REF AMDS 5300-2358). SPACER AT MID CARGO COMPARTMENT DOOR JAMB BEAM REPAIR ALSO THE REPAIR DOES NOT MEET REQUIREMENTS PER SRM, W
- [SDR DALA2017092006983](https://openairdocs.org/sdr/DALA2017092006983.md): Slide · low pressure · Sep 19, 2017 · N922DL · Doug MD88 · Escape Slide
  > LOW PRESSURE ON THE R1 SLIDE. THE R1 SLIDE WAS REPLACED IAW AMM 52-62-00.
- [SDR DALA2017091306874](https://openairdocs.org/sdr/DALA2017091306874.md): Angle · corroded · Sep 12, 2017 · N922DL · Doug MD88 · Fuselage Miscellaneous Structure
  > AWR.HIDDEN DAMAGE:THIS CARD IS ISSUED WITH THE CORRECT TEXT INSTEAD OF NRC 00805. CORROSION ON LH CUSP ANGLE BTW STA Y=218 TO Y=- 227 AND X=54 TO X=60 AT CABIN FLOOR STRUCTURE. PERMANENT REPAIR ON ANGLE CUSP WAS ACCOMPLISHED PER ETI-88-17-228 REV. 2. AND ER/A
- [SDR DALA2017091406878](https://openairdocs.org/sdr/DALA2017091406878.md): Angle · corroded · Sep 12, 2017 · N922DL · Doug MD88 · Fuselage Miscellaneous Structure
  > CORROSION ON CEILING SUPPORT ANGLE BS 1231, LBL 18 AND 32 IN THE AFT CARGO BAY. THE ANGLE WAS REPLACED IAW DWG 5956707, REV AT, SRM 51-10-3, 51-10-2, 51-10-4, 51-30-2, AND 51-30-5.
- [SDR DALA2017091306851](https://openairdocs.org/sdr/DALA2017091306851.md): Longeron Splice · cracked · Sep 12, 2017 · N922DL · Doug MD88 · Fuselage Main, Longeron/Stringer
  > CRACKED LONGERON SPLICE 22L BETWEEN BS 1271 TO 1287. THE LONGERON SPLICE WAS REMOVED AND REPLACED IAW SRM 53-02, FIG.18, 51-30-5, 51-10-3, & 51-10-4.
- [SDR DALA2017091206850](https://openairdocs.org/sdr/DALA2017091206850.md): Bulkhead · corroded · Sep 11, 2017 · N922DL · Doug MD88 · Fuselage Main, Bulkhead
  > CORROSION ON AFT BULKHEAD AT WALKING BRIDGE. THE BULKHEAD WAS REPLACED IAW SRM 51-30-2 AND DWG 9911993 REV CJ.
- [SDR DALA2017091206831](https://openairdocs.org/sdr/DALA2017091206831.md): Intercostal · corroded · Sep 11, 2017 · N922DL · Doug MD88 · Entrance Stairs
  > CORROSION ON INTERCOSTAL AT WALKING BRIDGE. THE INTERCOSTAL WAS REPLACED IAW SRM 51-30-2.
- [SDR DALA2017091206830](https://openairdocs.org/sdr/DALA2017091206830.md): Access Panel · corroded · Sep 11, 2017 · N922DL · Doug MD88 · Wing, Plate/Skin
  > CORROSION ON THE LT WING HEATER BLANKET FWD FUEL BOOST PUMP SECONDARY ACCESS COVER. FWD FUEL BOOST PUMP SECONDARY ACCESS COVER WAS REPLACED.
- [SDR DALA2017091006775](https://openairdocs.org/sdr/DALA2017091006775.md): Floor Support · damaged · Sep 10, 2017 · N922DL · Doug MD88 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT CORRODED AND CRACKED, BS 1287 TO 1307, BL 0. THE FLOOR SUPPORT WAS REPAIRED IAW SRM 53-01, FIG 4.
- [SDR DALA2017091006774](https://openairdocs.org/sdr/DALA2017091006774.md): Seat Track · corroded · Sep 9, 2017 · N922DL · Doug MD88 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION OUT OF LIMIT ON THE SEAT TRACK RBL 54, BS 790 - 796. THE SEAT TRACK WAS REPLACED IAW SRM 53-05, FIG 4F, 51-10-03, PAR 21, 14, AND 51-30-01.
- [SDR DALA2017091006771](https://openairdocs.org/sdr/DALA2017091006771.md): Door Frame · worn · Sep 9, 2017 · N922DL · Doug MD88 · Fuselage Main, Structure
  > WORN LEFT MLG WW DOOR FRAME AFT CHANNEL BS 937 AND LBL 60. MLG WW DOOR FRAME WAS REPLACED IAW SRM 51-30-2, 51-30-5, SRM 51-10-04, AND 51-10-3 PAR 14, 21.
- [SDR DALA2017090806750](https://openairdocs.org/sdr/DALA2017090806750.md): Support · corroded · Sep 7, 2017 · N922DL · Doug MD88 · Fuselage Miscellaneous Structure
  > CORROSION ON GIRT BAR SUPPORTS AT FWD GALLEY SERVICE ENTRACE DOOR. SUPPORTS AT FWD GALLEY SERVICE ENTRANCE DOOR WERE REPLACED. (LP# 0202940)
- [SDR DALA2017090806747](https://openairdocs.org/sdr/DALA2017090806747.md): Channel · cracked · Sep 7, 2017 · N922DL · Doug MD88 · Fuselage Floor Panel
  > CRACKED PREVIOUS REPAIR ON HAT CHANNEL AT FLOOR PANEL 927E. THE FLOOR PANEL WAS REPLACED IAW SRM 53-01, FIG 2.
- [SDR DALA2017090806742](https://openairdocs.org/sdr/DALA2017090806742.md): Access Panel · corroded · Sep 7, 2017 · N922DL · Doug MD88 · Wing, Plate/Skin
  > CORROSION ON FUEL TANK ACCESS PANEL 1367C. THE ACCESS PANEL WAS REPAIRED IAW SRM 51-22-2A, AND SRM 51-10-3, PAR 21.
- [SDR DALA2017090806737](https://openairdocs.org/sdr/DALA2017090806737.md): Angle · cracked · Sep 7, 2017 · N922DL · Doug MD88 · Cargo/Baggage Doors
  > CRACKED ANGLE AT BS 389 BETWEEN THE LOWER EDGE AND BEAM NR 1 ON THE FWD CARGO DOOR. THE ANGLE WAS REPLACED IAW SRM 51-30-2.
- [SDR DALA2017090706711](https://openairdocs.org/sdr/DALA2017090706711.md): Access Panel · corroded · Sep 6, 2017 · N922DL · Doug MD88 · Wing, Plate/Skin
  > CORROSION ON FUEL TANK ACCESS PLATES NBR 1371C, 1303C, 1335C. PANELS WERE REPLACED. (LP# 0201594)
- [SDR DALA2017090700004](https://openairdocs.org/sdr/DALA2017090700004.md): Frame · worn · Sep 6, 2017 · N922DL · Doug MD88 · Fuselage Main, Frame
  > WORN FRAME TEE BS 1380, LOWER FACE BETWEEN LONGERON 24L TO 24R AT AFT ACCESORY COMPARTMENT. REPLACED THE FRAME.
- [SDR DALA2017090706710](https://openairdocs.org/sdr/DALA2017090706710.md): Spacer · corroded · Sep 6, 2017 · N922DL · Doug MD88 · Fuselage Miscellaneous Structure
  > CORROSION ON SPACER AT THE AFT CARGO DOOR FRAME REPAIR, BS 1174 - 1212. REPAIRED IAW SRM 53-05, FIG 123, 51-10-3, PAR 14, 21, 38, SRM 51-30-5, AND 51-10-2.
- [SDR DALA2017090606672](https://openairdocs.org/sdr/DALA2017090606672.md): Angle · cracked · Sep 5, 2017 · N922DL · Doug MD88 · Fuselage Miscellaneous Structure
  > CRACKED ANGLE ON UPPER SURFACE BS 826, RBL 42. THE ANGLE WAS REPAIRED IAW ERA 498192-14MA, REV A.
- [SDR DALA2017090606667](https://openairdocs.org/sdr/DALA2017090606667.md): Skin · dented · Sep 5, 2017 · N922DL · Doug MD88 · Elevator, Tab Structure
  > DENTS ON THE UPPER & LOWER SURFACE SKIN OF THE LT ELEVATOR CONTROL TAB, AND THE ELEVATOR ANTI-FLOAT TAB. THE TAB SKIN WAS REPAIRED IAW SRM 55-04, PAR 3.
- [SDR DALA2017090606666](https://openairdocs.org/sdr/DALA2017090606666.md): Cusp Web · nicked · Sep 5, 2017 · N922DL · Doug MD88 · Fuselage Miscellaneous Structure
  > NICKS ON THE RT CUSP WEB BETWEEN BS 870 - 876, RBL 48 TO 52. THE CUSP WEB WAS REPAIRED IAW SRM 53-05, FIG 131A.
- [SDR DALA2017090606662](https://openairdocs.org/sdr/DALA2017090606662.md): Access Panel · corroded · Sep 5, 2017 · N922DL · Doug MD88 · Wing, Plate/Skin
  > CORROSION ON FUEL TANK ACCESS PLATES NR 1410C. FOUND OUT OF LIMITS AND REPLACED IAW SRM 51-22-2A,
- [SDR DALA2017090506606](https://openairdocs.org/sdr/DALA2017090506606.md): Cusp Web · corroded · Sep 4, 2017 · N922DL · Doug MD88 · Fuselage Miscellaneous Structure
  > CORROSION OUT OF LIMITS ON RT CABIN FLOOR MEMBRANE AT STA Y =662 TO Y=667 AND Y=680 TO Y=683 IN REF NRC 00285. CUSP WEB WAS REPAIRED PER SRM 51-70-4.
- [SDR DALA2017090506605](https://openairdocs.org/sdr/DALA2017090506605.md): Cusp Web · corroded · Sep 4, 2017 · N922DL · Doug MD88 · Fuselage Miscellaneous Structure
  > AFTER TO REMOVE CORROSION ON CUSP WEB BTW STA Y=1174 TO Y=1193, X=-54 TO X=-60, AREA WAS FOUND OUT OF LIMITS. CORROSION ON CUSP WEB BTW STA Y=1174 TO Y=1193, X=-54 TO X=-60 WAS REPAIRED PER SRM 51-70-04 FIG 2 (SHEET 1).
- [SDR DALA2017090406598](https://openairdocs.org/sdr/DALA2017090406598.md): Angle · cracked · Sep 3, 2017 · N922DL · Doug MD88 · Fuselage Miscellaneous Structure
  > CRACKED ANGLE AT BS 1338, LONGERON 7R AT THE AFT PRESURE BULKHEAD, THE ANGLE WAS REPAIRED IAW SRM 53-01, FIG 3.
- [SDR DALA2017090306594](https://openairdocs.org/sdr/DALA2017090306594.md): Cusp Web · corroded · Sep 2, 2017 · N922DL · Doug MD88 · Fuselage Miscellaneous Structure
  > CORROSION ON THE CUSP WEB BETWEEN BS 399 - 401, RBL 44 TO 60. THE CUSP WEB WAS REPAIRED IAW SRM 51-70-4.
- [SDR DALA2017090306539](https://openairdocs.org/sdr/DALA2017090306539.md): Cusp Web · nicked · Sep 2, 2017 · N922DL · Doug MD88 · Fuselage Miscellaneous Structure
  > TWO NICKS ON THE RT CABIN FLOOR CUSP WEB BETWEEN RBL 44 AND 54, BS 1054 TO 1063. THE CUSP WEB WAS REPAIRED IAW SRM 53-01, FIG 1.
- [SDR DALA2017090206530](https://openairdocs.org/sdr/DALA2017090206530.md): Cusp Web · corroded · Sep 1, 2017 · N922DL · Doug MD88 · Fuselage Miscellaneous Structure
  > CORROSION ON LT CABIN FLOOR CUSP WEB UPPER/LOWER SURFACE BTW LBL 54 AND 60 FROM BS 598 TO 712. THE CUSP WEB WAS REPLACED IAW SRM 53-05 FIG. 131A-24, AND SRM 51-30-01, 51-30-02, 51-30-05.
- [SDR DALA2017090106501](https://openairdocs.org/sdr/DALA2017090106501.md): Cusp Web · corroded · Aug 31, 2017 · N922DL · Doug MD88 · Fuselage Miscellaneous Structure
  > CORROSION ON RT CABIN FLOOR CUSP WEB UPPER/LOWER SURFACE BTW X=-44 AND X=-60 FROM STA Y=503 TO Y=598. SECTION CUSP WEB WAS REPLACE ON STA Y= 503 TO Y=598 BTW X=-44 AND X=-60 PER SRM 53-05 FIG 131A-16, 53-05 FIG131A-24 AND SRM 51-30-01,51-30-02, 51-30-05.
- [SDR DALA2017083106480](https://openairdocs.org/sdr/DALA2017083106480.md): Angle · corroded · Aug 30, 2017 · N922DL · Doug MD88 · Fuselage Miscellaneous Structure
  > CORROSION ON LT LOWER EPC ANGLE BS 160 AND LBL 50. THE ANGLE WAS REPLACED IAW SRM 51-30-2, 51-30-1, AND DWG 9955780, REV LA.
- [SDR DALA2017082900003](https://openairdocs.org/sdr/DALA2017082900003.md): Pin · corroded · Aug 28, 2017 · N922DL · Doug MD88 · Spoilers
  > CORROSION AND WORN RT AND LT INBD FLIGHT SPOILER HINGE CENTER PINS. THE PINS WERE REPLACED.
- [SDR DALA2017082900002](https://openairdocs.org/sdr/DALA2017082900002.md): Angle · cracked · Aug 28, 2017 · N922DL · Doug MD88 · Cargo/Baggage Doors
  > CRACKED ANGLE BETWEEN LOWER EDGE AND BEAM NR 1 AT AFT CARGO DOOR. THE ANGLE WAS REPLACED.
- [SDR DALA2017082900001](https://openairdocs.org/sdr/DALA2017082900001.md): Splice · corroded · Aug 28, 2017 · N922DL · Doug MD88 · Fuselage Miscellaneous Structure
  > CORROSION ON CUSP ANGLE SPLICE BETWEEN BS 503 - 522, RBL 60. THE CUSP SPLICE WAS REPLACED.
- [SDR DALA2017082806403](https://openairdocs.org/sdr/DALA2017082806403.md): Floor Panel · delaminated · Aug 27, 2017 · N922DL · Doug MD88 · Fuselage Floor Panel
  > DELAMINATION FLOOR PANEL NR 200E, 617C, 160E AT PASSENGER CABIN. FLOOR PANEL NR 200E, 617C AND 160E WERE REMPLACED AND IDENTIFIED PER AMM 53-20-01-201.
- [SDR DALA2017082806402](https://openairdocs.org/sdr/DALA2017082806402.md): Skin · damaged · Aug 27, 2017 · N922DL · Doug MD88 · Rudder, Plate/Skin
  > DAMAGE METALIZED COAT ON RUDDER SKIN LT AND RT SIDE. RUDDER WAS REPAIRED PER SRM 51-70-1A PAR 23 AND ERA 092613-14MA REV A.
- [SDR DALA2017082706401](https://openairdocs.org/sdr/DALA2017082706401.md): Skin · dented · Aug 26, 2017 · N922DL · Doug MD88 · Elevator, Tab Structure
  > DENTS DAMAGE ON UPPER/LOWER SURFACE SKIN AT LT ELEVATOR GEARED TAB, ALSO DEGRADED SEALANT. ELEVATOR GEARED TAB LT WAS REPAIRED PER SRM 55-04 PAR 2 C AND SRM 51-20-0.
- [SDR DALA2017082606400](https://openairdocs.org/sdr/DALA2017082606400.md): Pan · cracked · Aug 25, 2017 · N922DL · Doug MD88 · Fuselage Miscellaneous Structure
  > CRACK ON RING PAN UPPER FWD CORNER STA Y=846 LEFT SIDE. RING PAN UPPER FWD CORNER STA Y=846 LEFT SIDE WAS REPAIRED PER SRM 53-05 FIG 122 AND 51-10-03.

Next page: https://openairdocs.org/deregistered/N922DL-2022-09-20/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 = 'N922DL' AND deregistration_id = 'N922DL-2022-09-20'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N922DL-2022-09-20/reports

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