# Service difficulty reports: N905DE, cancelled Nov 29, 2022

A list on [N905DE, cancelled Nov 29, 2022](https://openairdocs.org/deregistered/N905DE-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 · 154 reports

- [SDR DALA2019101605927](https://openairdocs.org/sdr/DALA2019101605927.md): Switch · malfunctioned · Oct 16, 2019 · N905DE · Doug MD88 · Stabilizer Position Indicating
  > SHIP 9005 - ATO - REJECTED TAKE-OFF AT 110 KNOTS DUE TO STABILIZER CONFIGURATION WARNING. CORRECTIVE ACTION: REPLACED HORIZONTAL STAB SWITCH (S1-491) AND CAW UNIT - C/W NO-GO-ODI TASKS.
- [SDR DALA2019060323357](https://openairdocs.org/sdr/DALA2019060323357.md): Generator · disconnected · Jun 1, 2019 · N905DE · Doug MD88 · AC Generator-Alternator
  > AT 12,000 MSL, AUTO THROTTLES/AUTOPILOT DISCONNECTED L AC BUSS OFF, AND AC CROSS TIE LOCKOUT, L GEN OFF STALL IND FAIL, ON OAP, RAN QRH FOR LAC BUS OFF & AC CROSSTIE LOCKOUT. STARTED TO DESCEND AND CONFIGURE FOR LANDING AT FLAPS 15 GEAR DOWN, WE NOTICED THERE
- [SDR DALA2018091805641](https://openairdocs.org/sdr/DALA2018091805641.md): Channel · cracked · Sep 17, 2018 · N905DE · Doug MD88 · Engine Cowling System
  > CHANNEL CRACKED TWO PLACES AFT SIDE OF NOSE COWL AFT BULKHEAD 6 O'CLOCK POSITION. REPLACED NR 1 NOSE COWL REF AMM 71-10-01.
- [SDR DALA2018090405399](https://openairdocs.org/sdr/DALA2018090405399.md): Slide · unsecure · Sep 1, 2018 · N905DE · Doug MD88 · Escape Slide
  > L1 DOOR SLIDE PIN PULLED AND SLIDE PACKAGE STARTED TO OPEN. R&R L1 DOOR SLIDE PER W/C 2561-01358-04A.
- [SDR DALA2018052903616](https://openairdocs.org/sdr/DALA2018052903616.md): Lamp · inoperative · May 29, 2018 · N905DE · Doug MD88 · Emergency Lighting
  > EMERGENCY LIGHTS WERE INOPERATIVE AT 1CD. REPLACED THE LAMP. OPS CHECKED GOOD.
- [SDR DALA2018030701444](https://openairdocs.org/sdr/DALA2018030701444.md): Slide · low pressure · Mar 4, 2018 · N905DE · Doug MD88 · Escape Slide
  > R1 DOOR SLIDE PRESSURE OUTSIDE OF GREEN RANGE. REPLACED THE SERVICE DOOR SLIDE IAW WORK CARD 2561-4964.
- [SDR DALA2018010200008](https://openairdocs.org/sdr/DALA2018010200008.md): Light · inoperative · Dec 30, 2017 · N905DE · Doug MD88 · Emergency Lighting
  > L1 DOOR EMERG LIGHT INOP. RELAMPED IAW AMM 33-50.
- [SDR DALA2017081806299](https://openairdocs.org/sdr/DALA2017081806299.md): Battery Pack · inoperative · Aug 18, 2017 · N905DE · Doug MD88 · Emergency Lighting
  > EMERGENCY LIGHTS ROWS 22-25 CELING INOPERATIVE. R & R THE BATTERIES IN B5104. OPS CHECKED GOOD.
- [SDR DALA2017022301496](https://openairdocs.org/sdr/DALA2017022301496.md): Sensor · loose · Feb 21, 2017 · N905DE · Doug MD88 · Windshield/Door Rain/Ice Removal
  > DURING TAXI IN, FIRST OFFICER`S WINDSHIELD HAD A LARGE SPARK. WINDSHIELD HEAT IS NO LONGER FUNCTIONING. FOUND THE WINDOW ANTI-FOG SENSOR LOOSE AND IN CONTACT WITH MOUNT SPRING. SECURED AND TESTED IAW AMM 30-41-01. OK FOR SERVICE.
- [SDR DALA2017011800478](https://openairdocs.org/sdr/DALA2017011800478.md): Battery Pack · inoperative · Jan 17, 2017 · N905DE · Doug MD88 · Emergency Lighting
  > COCKPIT EMERGENCY LIGHTS WERE INOPERATIVE. REPLACED THE BATTERY PACK AND TESTED IAW AMM 33-53. OPS CHECKED OK.
- [SDR DALA2016081706054](https://openairdocs.org/sdr/DALA2016081706054.md): Lanyard · damaged · Aug 16, 2016 · N905DE · Doug MD88 · Escape Slide
  > DAMAGE IN L1 SLIDE RELEASE LANYARD CABLE. L1 RELEASE LANYARD CABLE WAS REPLACED IAW AMM 25-62-01.
- [SDR DALA2016081405973](https://openairdocs.org/sdr/DALA2016081405973.md): Stringer · cracked · Aug 13, 2016 · N905DE · Doug MD88 · Fuselage Main, Longeron/Stringer
  > CRACK OF 0.750" WAS FOUND ON STRINGER 17R. REPAIRED PER ERA 547891-14AD REV. ORG. AND ERA 547892-14 REV. ORG..
- [SDR DALA2016081205954](https://openairdocs.org/sdr/DALA2016081205954.md): Frame · cracked · Aug 11, 2016 · N905DE · Doug MD88 · Fuselage Main, Frame
  > INITIAL INSPECTION CRACK ON FRAME OF CANT STA Y=1510 BETWEEN 12:00 TO 1:00 POSITION AT AFT ACCESSORIES COMPARTMENT. FRAME WAS REPLACED IAW SRM 51-30-2 AND DWG 9911843.
- [SDR DALA2016081205953](https://openairdocs.org/sdr/DALA2016081205953.md): Floor Panel · damaged · Aug 11, 2016 · N905DE · Doug MD88 · Fuselage Floor Panel
  > ELONGATED HOLES ON GENERATION FLOOR PANEL NR 826G, 389G AND 769G. DUE TO EXCESSIVE ELONGATED HOLE FLOOR PANEL 769G WAS REPAIRED IAW SRM 51-70-4, FIG 1, SH 2 FLOOR PANEL 826G HOLES WERE DRILLED TO NEXT OVERSIZED IAW SRM 51-10-4, FLOOR PANEL 389G WILL BE REPLAC
- [SDR DALA2016081105935](https://openairdocs.org/sdr/DALA2016081105935.md): Cargo Track · corroded · Aug 10, 2016 · N905DE · Doug MD88 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON LEFT CARGO TRACK BETWEEN BS 1145 - 1222. THE CARGO TRACK WAS REPLACED IAW SRM 51-30-2, SRM 51-30-1 AND DWG 5936663 REV "Y".
- [SDR DALA2016081105934](https://openairdocs.org/sdr/DALA2016081105934.md): Cargo Track · corroded · Aug 10, 2016 · N905DE · Doug MD88 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON RIGHT CARGO TRACK BETWEEN BS 1145 - 1155. THE CARGO TRACK WAS REPLACED IAW DWG 5936663 REV "Y", SRM 51-10-1 AND 51-30-2.
- [SDR DALA2016081105933](https://openairdocs.org/sdr/DALA2016081105933.md): Access Panel · corroded · Aug 10, 2016 · N905DE · Doug MD88 · Wing, Plate/Skin
  > CORROSION ON FUEL ACCESS PANEL 1331C. THE ACCESS PANEL WAS REPLACED IAW AMM 20-30-01.
- [SDR DALA2016081105929](https://openairdocs.org/sdr/DALA2016081105929.md): Cargo Track · corroded · Aug 10, 2016 · N905DE · Doug MD88 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON RIGHT CARGO TRACK FROM BS 1231 - 1322. THE CARGO TRACK WAS REPLACED IAW SRM 51-30-2, SRM 51-30-1. SRM, 51-10-4, SRM.51-10-3 PAR. 14-21 AND DWG 5936660 REV, BZ.
- [SDR DALA2016081105928](https://openairdocs.org/sdr/DALA2016081105928.md): Cargo Track · corroded · Aug 10, 2016 · N905DE · Doug MD88 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON LEFT CARGO TRACK BS 1221 - 1322. CARGO TRACK WAS REPLACED IAW DWG 5936660 REV BZ.
- [SDR DALA2016081005917](https://openairdocs.org/sdr/DALA2016081005917.md): Access Panel · corroded · Aug 9, 2016 · N905DE · Doug MD88 · Wing, Plate/Skin
  > CORROSION ON COUNTERSINK AND SETTLEMENT AREA ON FUEL ACCESS PANEL 1311C ON LT WING. THE ACCESS PANEL WAS REPLACED.
- [SDR DALA2016080905886](https://openairdocs.org/sdr/DALA2016080905886.md): Doubler · corroded · Aug 8, 2016 · N905DE · Doug MD88 · Fuselage Main, Plate/Skin
  > CORROSION ON INTERNAL DOUBLER AT INNER FUSELAGE MID CARGO BAY BETWEEN BS 636 - 645 LONGERON 29R AND 29L. THE DOUBLER WAS REPLACED IAW SRM 51-10-4, 51-10-3 PAR 14 AND 21, 51-30-2, 51-30-5 AND DWG. 5911412 REV. DU.
- [SDR DALA2016080805858](https://openairdocs.org/sdr/DALA2016080805858.md): Longeron · corroded · Aug 8, 2016 · N905DE · Doug MD88 · Fuselage Main, Longeron/Stringer
  > CORROSION ON LONGERON 22L BETWEEN BS 1287 - 1309. THE LONGERON WAS FOUND OUT LIMITS AND REPAIRED IAW 53-02 FIG 18.
- [SDR DALA2016080805859](https://openairdocs.org/sdr/DALA2016080805859.md): Pan · cracked · Aug 6, 2016 · N905DE · Doug MD88 · Cargo/Baggage Doors
  > CRACKED FWD EDGE PAN ON FWD CARGO DOOR OVER BEAM NR 5. THE EDGE PAN WAS REPAIRED IAW SRM 53-05D FIG.
- [SDR DALA2016080605853](https://openairdocs.org/sdr/DALA2016080605853.md): Cusp Web · cracked · Aug 5, 2016 · N905DE · Doug MD88 · Fuselage Miscellaneous Structure
  > A CRACK WAS FOUND ON LT CUSP WEB BETWEEN BS 845 - 864 AND X 44 TO X 60. THE CUSP WEB WAS REPAIRED IAW SRM 53-05 FIG 131A-10.
- [SDR DALA2016080505784](https://openairdocs.org/sdr/DALA2016080505784.md): Stringer · cracked · Aug 4, 2016 · N905DE · Doug MD88 · Fuselage Main, Longeron/Stringer
  > CRACKED STR NR 20 LT STA Y, 1003 ABOVE TRAPEZOIDAL PANEL AT LT WHEEL WELL. STRINGER NR 20 WAS REPAIRED IAW SRM 53-02, FIG 22.
- [SDR DALA2016080405769](https://openairdocs.org/sdr/DALA2016080405769.md): Skin · cracked · Aug 3, 2016 · N905DE · Doug MD88 · Cargo/Baggage Doors
  > CRACK ON OUTER SKIN BETWEEN BEAMS NR 1 TO 2 AND PROJECTION STA Y:658 OF AFT MID CARGO COMPARTMENT DOOR. SKIN WAS REPAIRED IAW ERA 486446-14MA, REV ORIGINAL.
- [SDR DALA2016080405767](https://openairdocs.org/sdr/DALA2016080405767.md): Longeron · cracked · Aug 3, 2016 · N905DE · Doug MD88 · Fuselage Main, Longeron/Stringer
  > INITIAL INSPECTION, CRACK ON LONG 4RT AND STA Y=1437 AT AFT ACCESSORIES COMPARTMENT. LONGERON WAS REPAIRED IAW SRM 53-02, FIG 18.
- [SDR DALA2016080405766](https://openairdocs.org/sdr/DALA2016080405766.md): Longeron · cracked · Aug 3, 2016 · N905DE · Doug MD88 · Fuselage Main, Longeron/Stringer
  > INITIAL INSPECTION, CRACK ON LONG 3LT AND STA Y=1437 AT AFT ACCESSORIES COMPARTMENT. LONGERON WAS REPAIRED IAW SRM 53-02, FIG 18.
- [SDR DALA2016080405764](https://openairdocs.org/sdr/DALA2016080405764.md): Skin · cracked · Aug 3, 2016 · N905DE · Doug MD88 · Fuselage Main, Plate/Skin
  > CRACK OF 0.062" ON FUSELAGE SKIN AT THE UPPER FWD DOOR JAMB CORNER STA Y=375.5 BETWEEN LONG 19-20 RT OF THE FWD CARGO COMPARTMENT. FUSELAGE SKIN AT THE UPPER FWD DOOR JAMB CORNER STA Y= 375.5 BETWEEN LONGERON 19-20 RT OF THE FWD CARGO COMPARTMENT WAS REPAIRED
- [SDR DALA2016080305732](https://openairdocs.org/sdr/DALA2016080305732.md): Beam · cracked · Aug 2, 2016 · N905DE · Doug MD88 · Cargo/Baggage Doors
  > CRACK ON BEAM NR 5 AND BS 427 OF FWD CARGO DOOR. THE BEAM WAS REPLACED IAW SRM 51-30-2 AND 51-30-5.
- [SDR DALA2016080305729](https://openairdocs.org/sdr/DALA2016080305729.md): Access Panel · corroded · Aug 2, 2016 · N905DE · Doug MD88 · Wing, Plate/Skin
  > CORROSION ON COUNTERSINKS AND SETTLEMENT AREA ON FUEL ACCESS PANEL 1335. ACCESS PANEL WAS REPLACED.
- [SDR DALA2016080305728](https://openairdocs.org/sdr/DALA2016080305728.md): Access Panel · corroded · Aug 2, 2016 · N905DE · Doug MD88 · Wing, Plate/Skin
  > CORROSION ON COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCESS PANEL 1414C ON RT WING. THE ACCESS PANEL WAS REPLACED.
- [SDR DALA2016080305724](https://openairdocs.org/sdr/DALA2016080305724.md): Angle · cracked · Aug 2, 2016 · N905DE · Doug MD88 · Emergency Exits
  > CRACKED ANGLE ON DOOR STOP AT RT AFT OVERWING EMERGENCY EXIT. THE ANGLE WAS REPLACED IAW DWG 9957735 REV. G AND SRM 51-30-5 AND 51-30-2.
- [SDR DALA2016080305723](https://openairdocs.org/sdr/DALA2016080305723.md): Door Frame · cracked · Aug 2, 2016 · N905DE · Doug MD88 · Fuselage Main, Structure
  > CRACK ON EMERGENCY EXIT DOOR FRAME (UPPER AREA) BS 919 LT SIDE. THE DOOR FRAME WAS REPAIRED IAW SRM 53-05 FIG.32.
- [SDR DALA2016080205714](https://openairdocs.org/sdr/DALA2016080205714.md): Frame · cracked · Aug 2, 2016 · N905DE · Doug MD88 · Fuselage Main, Frame
  > CRACK ON FRAME BS 1322 LONGERON 17R. THE FRAME WAS REPAIRED IAW ER 493697-14MA REV. B.
- [SDR DALA2016080205712](https://openairdocs.org/sdr/DALA2016080205712.md): Floor Panel · damaged · Aug 1, 2016 · N905DE · Doug MD88 · Fuselage Floor Panel
  > DAMAGED FERRULS ON FLOOR PANEL. FLOOR PANEL REPAIRED IAW AMM 53-20-01-201 AND AMM 88 53-20-01-201.
- [SDR DALA2016080205711](https://openairdocs.org/sdr/DALA2016080205711.md): Longeron · cracked · Aug 1, 2016 · N905DE · Doug MD88 · Fuselage Main, Longeron/Stringer
  > CRACK FOUND ON LONGERON 16L, BS 1437. THE LONGERON WAS REPLACED IAW SRM 53-14-4 FIG 4, SRM 51-30-5, AND SRM 51-30-2.
- [SDR DALA2016080105699](https://openairdocs.org/sdr/DALA2016080105699.md): Cusp Web · cracked · Jul 31, 2016 · N905DE · Doug MD88 · Fuselage Miscellaneous Structure
  > CRACK ON LEFT CUSP WEB BS 905 - 927, X 54 - 60. THE CUSP WEB WAS REPAIRED IAW SRM 53-05 FIG. 131A-14 51-30-2, 51-30-5, AND 51-10-3 PAR. 14,21 & 38.
- [SDR DALA2016080105709](https://openairdocs.org/sdr/DALA2016080105709.md): Cusp Web · corroded · Jul 30, 2016 · N905DE · Doug MD88 · Fuselage Miscellaneous Structure
  > CORROSION ON RT CUSP WEB BS 1003 - 1020. THE CUSP WEB WAS REPAIRED IAW SRM 51-30-2, 53-05 FIG. 131A-14, 51-10-3 PAR. 21,14 AND 51-30-5 CABIN.
- [SDR DALA2016080105708](https://openairdocs.org/sdr/DALA2016080105708.md): Cusp Web · corroded · Jul 30, 2016 · N905DE · Doug MD88 · Fuselage Miscellaneous Structure
  > CORROSION ON PREVIOUS REPAIR DOUBLER ON LT CUSP WEB BS 934 - 946, X 54-60. REPAIRED IAW SRM 53-05 FIG 131. AND 51-30-2.
- [SDR DALA2016080105707](https://openairdocs.org/sdr/DALA2016080105707.md): Cusp Web · corroded · Jul 30, 2016 · N905DE · Doug MD88 · Fuselage Miscellaneous Structure
  > CORROSION ON RT CUSP WEB BS 1060 - 1079. CUSP WEB REPAIRED IAW SRM 53-05 FIG. 131A-14 AND SRM 51-30-5.
- [SDR DALA2016080105706](https://openairdocs.org/sdr/DALA2016080105706.md): Cusp Web · corroded · Jul 30, 2016 · N905DE · Doug MD88 · Fuselage Miscellaneous Structure
  > CORROSION ON RT CUSP WEB BS 1041 - 1050. THE CUSP WEB WAS REPAIRED IAW SRM 53-05 FIG. 131A-13.
- [SDR DALA2016080105703](https://openairdocs.org/sdr/DALA2016080105703.md): Angle · cracked · Jul 30, 2016 · N905DE · Doug MD88 · Passenger/Crew Doors
  > CRACK ON ANGLE BEAM FWD AT FWD ENTRY DOOR. ANGLE WAS REPLACED IAW SRM 51-30-2, 51-30-5, AND DWG 9955752 REV M.
- [SDR DALA2016080105702](https://openairdocs.org/sdr/DALA2016080105702.md): Rib · cracked · Jul 30, 2016 · N905DE · Doug MD88 · Wing, Rib/Bulkhead
  > CRACK ON RIB XOS 455 ON RT WING FIXED LE STRUCTURE. THE RIB WAS REPAIRED IAW SRM 57-06B D FIG. 12 SHEET 4.
- [SDR DALA2016073105662](https://openairdocs.org/sdr/DALA2016073105662.md): Cusp Web · corroded · Jul 30, 2016 · N905DE · Doug MD88 · Fuselage Miscellaneous Structure
  > CORRODED PREVIOUS REPAIR DOUBLER ON LT CUSP WEB BETWEEN BS 446 - 459, X 54 - 60. THE DOUBLER WAS REPLACED IAW SRM 53-05 FIGURE 131A-2.
- [SDR DALA2016073105661](https://openairdocs.org/sdr/DALA2016073105661.md): Cusp Web · corroded · Jul 30, 2016 · N905DE · Doug MD88 · Fuselage Miscellaneous Structure
  > CORRODED REPAIR DOUBLERS ON LT CUSP WEB BETWEEN BS 984 - 1003, AND BS 1003 - 1022, X 54 - 60. REPAIR REPLACED IAW SRM 53-05 FIG. 131A-4, 131A-6, 51-10-3 PAR. 14,21,38, 51-30-2 AND 51-30-5.
- [SDR DALA2016073105660](https://openairdocs.org/sdr/DALA2016073105660.md): Cusp Web · corroded · Jul 30, 2016 · N905DE · Doug MD88 · Fuselage Miscellaneous Structure
  > CORROSION ON LT CUSP WEB BETWEEN BS 965 - 984 AND X 54 - 60. THE CUSP WEB WAS REPAIRED IAW SRM 53-05 FIGURE 131A-2.
- [SDR DALA2016080105710](https://openairdocs.org/sdr/DALA2016080105710.md): Doubler · corroded · Jul 29, 2016 · N905DE · Doug MD88 · Fuselage Main, Plate/Skin
  > CORROSION ON REPAIR DOUBLER BS 446 - 465 AND X -44 TO -60. AREA WAS REPAIRED IAW SRM 53-05 FIG.131A-11, 51-10-3, 51-30-1, 51-30-2 & 51-30-5.
- [SDR DALA2016080105700](https://openairdocs.org/sdr/DALA2016080105700.md): Longeron · cracked · Jul 29, 2016 · N905DE · Doug MD88 · Fuselage Main, Longeron/Stringer
  > CRACK ON LONGERON 3R BS 1437. THE LONGERON WAS REPAIRED IAW SRM 53-02 FIG.18.
- [SDR DALA2016080105692](https://openairdocs.org/sdr/DALA2016080105692.md): Cusp Web · cracked · Jul 29, 2016 · N905DE · Doug MD88 · Fuselage Miscellaneous Structure
  > CRACK ON LT CUSP WEB OF STA Y642 BETWEEN STA X54 TO X60 AT PAX CABIN. REPAIRED IAW SRM 53-05 FIG 131A-14, 51-30-2, 51-10-3 PAR 21,14, 51-30-5 AND 51-10-3.

Next page: https://openairdocs.org/deregistered/N905DE-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 = 'N905DE' AND deregistration_id = 'N905DE-2022-11-29'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N905DE-2022-11-29/reports

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