# Service difficulty reports: N907DE, cancelled Nov 29, 2022

A list on [N907DE, cancelled Nov 29, 2022](https://openairdocs.org/deregistered/N907DE-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 · 179 reports

- [SDR DALA2020022631446](https://openairdocs.org/sdr/DALA2020022631446.md): Skin · cracked · Feb 22, 2020 · N907DE · Doug MD88 · Vertical Stabilizer, Plate/Skin
  > A/C DUE ERA 585429-14AD PRI REV O. VERTICAL STABILIZER LEADING EDGE ZFS 52.267 FRONT SPAR CAP DORSAL / LOWER ASSEMBLY LHS CRACK INDICATION. C/W ERA 585429-14AD REV ORIGINAL SECTION 1 PERMANENT REPAIR. (LP1500936)
- [SDR DALA2020022301342](https://openairdocs.org/sdr/DALA2020022301342.md): Skin · cracked · Feb 22, 2020 · N907DE · Doug MD88 · Vertical Stabilizer, Plate/Skin
  > /H VERTICAL STAB HAS CRACK INDICATION IN 6TH HOLE UP FROM STATION ZFS=52.267 ON FRONT SPAR CAP. REMOVED VERT STAB PER MD 88 AMM 55-30-01 THRU STEP 3(A)(7). REAMED HOLE IN VERTICAL SPAR CAP TO.233. PERFORMED BHEC PER MD88 NDTSPM PART 6-10-01.003 AND AMDS CARD
- [SDR DALA2020022101313](https://openairdocs.org/sdr/DALA2020022101313.md): Spar Cap · cracked · Feb 20, 2020 · N907DE · Doug MD88 · Vertical Stabilizer, Spar/Rib
  > VERTICAL STABILIZER LEADING EDGE SPAR CAP CARCK. REPETITIVE INSPECTION NEEDS TO BE PERFORMED EVERY 3000 FLIGHT CYCLES, THIS IS INCORPORATED INTO ER/A 585429-14. (LP1497972)
- [SDR DALA2019122407524](https://openairdocs.org/sdr/DALA2019122407524.md): Windshield Wiper · detached · Dec 23, 2019 · N907DE · Doug MD88 · Windshield/Door Rain/Ice Removal
  > CAPTAIN'S WINDSHIELD WIPER IS MISSING. FELL OFF ON SHORT FINAL. REPLACED THE WINDSHIELD WIPER ARM AND BLADE IAW AMM 30-42, OPS CKECKED GOOD.
- [SDR DALA2019081204697](https://openairdocs.org/sdr/DALA2019081204697.md): Landing Light · missing · Aug 11, 2019 · N907DE · Doug MD88 · Exterior Lighting
  > ON WALK AROUND, NOSE GEAR LANDING LIGHT ON F/O SIDE MISSING, WIRES HANGING OUT. FOUND RT TAXI LIGHT BULB AND RETAINING RING MISSING. INSTALLED NEW BULB REF MD88 AMM 33-41. SECURED BULB PER MEL 33-00-07C. C/B L-14 PULLED AND COLLARED PER RI 580440-14. NEW BULB
- [SDR DALA2019081104692](https://openairdocs.org/sdr/DALA2019081104692.md): Battery Pack · inoperative · Aug 11, 2019 · N907DE · Doug MD88 · Emergency Lighting
  > O/H EMERGENCY LIGHTS INOPERATIVE FROM ROW 16-29. REPLACED BATTERY PACKS B5-104 AND B5-102. OPS CHECKED GOOD IAW AMM 33-53.
- [SDR DALA2019080604589](https://openairdocs.org/sdr/DALA2019080604589.md): Terminal · shorted · Aug 5, 2019 · N907DE · Doug MD88 · Ice/Rain Protection System Wiring
  > TAXING INTO RAMP, BIG SPARK OUT OF CAPT WINDSHIELD ANTI-ICE CONNECTOR. FOUND WIRE TERMINAL IN CONTACT WITH SPRING ON WINDOW TEMP SENSOR. ADJUSTED WIRE TERMINAL FOR CLEARANCE. CKS OK. (LP5490390)
- [SDR DALA2019062503831](https://openairdocs.org/sdr/DALA2019062503831.md): Skin · damaged · Jun 24, 2019 · N907DE · Doug MD88 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN DAMAGE AT BS 180. REPAIRED THE SKIN IAW SRM 53-04-3.
- [SDR DALA2019041502421](https://openairdocs.org/sdr/DALA2019041502421.md): Battery Pack · inoperative · Apr 15, 2019 · N907DE · Doug MD88 · Emergency Lighting
  > BOTH FWD OVERWING EXIT DOOR EMERGENCY LTS INOP. R/R BATTERIES FOR FWD OVERWING DOOR LTS. OPS CHECK OK. BATTERIES R/R PER AMM 33-53.
- [SDR DALA2019021220917](https://openairdocs.org/sdr/DALA2019021220917.md): Structure · missing · Feb 11, 2019 · N907DE · Doug MD88 · Rudder Structure
  > DURING PAINT VISIT, FOUND RUDDER TO HAVE MISSING FLAME SPRAY. RUDDER P/N SN5955501-1 S/N 403. REMOVED AND REPLACE RUDDER WITH SERVICEABLE REDDER PER WORK CARD 2720-4421. RUDDER, ASSEMBL OFF 88-5554-9-0005 00403 ON 88-5554-9-0005 49321. (LP0941022)
- [SDR DALA2019010800100](https://openairdocs.org/sdr/DALA2019010800100.md): Controller · failed · Jan 8, 2019 · N907DE · Doug MD88 · Cabin Pressure Controller
  > BOTH AUTO PRESSURIZATION SYSTEMS FAILED DURING DESCENT AT APPROXIMATELY 22000 FEET RESULTING IN CABIN PRESSURE LOSS. REMOVED AND REPLACED A/C MOTOR DRIVE ASSY, NR 1 & NR 2 PRESSURE CONTROLLERS AND ADJUSTED AFT OUTFLOW VALVE PER AMM 21-32 AND TSM 21-32. PERFORM
- [SDR DALA2018103106351](https://openairdocs.org/sdr/DALA2018103106351.md): Unknown · haze · Oct 30, 2018 · N907DE · Doug MD88 · Air Distribution System
  > RIGHT AFTER GEAR RETRACTION BOTH AFT LABS SMOKE ALARMS STARTED BEEPING. NO SMOKES, LIGHT HAZE AND BURNING SMELL-LIGHT TO MEDIUM. WE COULD SMELL IN THE COCKPIT. AFTER 2 MINUTES THE ALARMS STOPPED & SMELL,HAZE DISSIPATED. AT LANDING AFTER STARTING APE SMELL CAM
- [SDR DALA2018102606300](https://openairdocs.org/sdr/DALA2018102606300.md): Skin · corroded · Oct 25, 2018 · N907DE · Doug MD88 · Fuselage Main, Plate/Skin
  > EVIDENCE OF CORROSION FOUND ON REPAIR EDGE AT AFT LAVATORY SERVICE PANEL- MARKED. SKIN/REPAIR BULGING OUT AT LOWER END OF CUTOUT. REPAIRED PER PRI 485410-14 REV A REV 0-3 MATCH ERA 485410-14 REV A. (LP0800060)
- [SDR DALA2018102606299](https://openairdocs.org/sdr/DALA2018102606299.md): Channel · damaged · Oct 25, 2018 · N907DE · Doug MD88 · Spoilers
  > AIRCRAFT DAMAGE: LT IB FLIGHT SPOILER HAT CHANNEL DAMAGED FROM SPOILER TORSION BAR REACTION BOLT. REPAIRED PER PRI 572530-14 REV O MATCHES ERA 572530-14 REV O. (LP0799992)
- [SDR DALA2018102406265](https://openairdocs.org/sdr/DALA2018102406265.md): Frame · cracked · Oct 23, 2018 · N907DE · Doug MD88 · Fuselage Main, Frame
  > STA 886 RT MAIN FRAME FOUND TO BE CRACKED THROUGH HFEC INSPECTION PERFORMED ON ROUTINE CARD 5310-01415-04D. REPLACED MAIN FRAME AT STA 886 RT PER 5310-01415-0302.
- [SDR DALA2018081505090](https://openairdocs.org/sdr/DALA2018081505090.md): Battery Pack · inoperative · Aug 15, 2018 · N907DE · Doug MD88 · Emergency Lighting
  > OVERHEAD EMERGENCY LIGHTS INOPERATIVE FROM SEATS 17 - 26 WERE INOPERATIVE. R & R THE BATTERY PACKS IAW AMM 33-53. OPS CHECKED GOOD.
- [SDR DALA2018062304167](https://openairdocs.org/sdr/DALA2018062304167.md): Smoke Detector · malfunctioned · Jun 22, 2018 · N907DE · Doug MD88 · Smoke Detection
  > LAVATORY (AFT RT) SMOKE DETECTOR WILL NOT SHUT OFF. R&R AFT RT LAV SMOKE DETECTOR AND BATT, CKS OK. REF AMM 26- 7.
- [SDR DALA2017122608876](https://openairdocs.org/sdr/DALA2017122608876.md): Wire · broken · Dec 25, 2017 · N907DE · Doug MD88 · Navigation System Wiring
  > EMERGENCY NAV INSTRUMENT CIRCUIT BREAKER TRIPPED. NO RESET. FOUND A WIRE 1F700A24 BROKEN AND ARCING. REPAIRED THE WIRE IAW MM 20. OPS NORMAL.
- [SDR DALA2017072105598](https://openairdocs.org/sdr/DALA2017072105598.md): Wire · broken · Jul 21, 2017 · N907DE · Doug MD88 · Light System Wiring
  > MIDDLE EMERGENCY LIGHT ON CATWALK INOPERATIVE. TERMINATED A BROKEN WIRE ON CATWALK EMERGENCY LIGHT IAW SWPM 20 AND EWIS. OPS CHECKED GOOD.
- [SDR DALA2017070505219](https://openairdocs.org/sdr/DALA2017070505219.md): Firewall · worn · Jul 4, 2017 · N907DE · Doug MD88 · Nacelle/Pylon, Bulkhead/Firewall
  > NR 2 ENGINE FIREWALL PASS THRU WORN AT PREVIOUS REPAIR LOCATED AT HYD PRESS LINE. SAME AREA HYD PRESS LINE LOOSE. FOUND DOUBLER AT PASS THRU FOR HYD LINES WORN. REMOVED OLD DOUBLER AND BAD HYD LINE. INSTALLED NEW DOUBLER IAW ERA 553921-14 REV ORIG. REINST
- [SDR DALA2017042403324](https://openairdocs.org/sdr/DALA2017042403324.md): Switch · failed · Apr 21, 2017 · N907DE · Doug MD88 · Aerodynamic Fairings
  > DURING FUNCTIONAL CHECK OF TAILCONE RELEASE SYSTEM USING AFT PASSENGER ENTRANCE DOOR EMERGENCY HANDLE, AFTER TAILCONE RELEASED FROM ACFT A TAILCONE UNSAFE MESSAGE ON EOAP PANEL IN FLIGHT COMPARTMENT FAILED TO COME ON. REPLACED THE SWITCH S1-538 IAW WDM 52-73-
- [SDR DALA2017021901359](https://openairdocs.org/sdr/DALA2017021901359.md): Line · no test · Feb 18, 2017 · N907DE · Doug MD88 · Extinguishing System
  > FOUND THREE FIRE EXTINGUISHER SUPPLY FLEX LINES BAD DURING A EXTINGUISHING LINE LEAK TEST IAW AMM 26-20-01-201. REPLACED THE LINES. (LP9119701)
- [SDR DALA2016111909007](https://openairdocs.org/sdr/DALA2016111909007.md): Indicator · malfunctioned · Nov 18, 2016 · N907DE · Doug MD88 · Landing Gear Position and Warning
  > NOSE GEAR LIGHT WOULD NOT ILLUMINATE WITH GEAR LEVER DOWN. NLG INDICATOR PIN EXTENDED. LIGHT TESTED OK. NLG LIGHT ILLUMINATED GREEN AFTER APPROX. 3 MINUTES FLYING AT 180KIAS. REPLACED WARN LIGHT DIM AND TEST UNIT 2 RELAY B5-75 IAW WDM 32-61-00.
- [SDR DALA2016100307008](https://openairdocs.org/sdr/DALA2016100307008.md): Pan · cracked · Oct 1, 2016 · N907DE · Doug MD88 · Cargo/Baggage Doors
  > CRACK ON LOWER PAN AFT EDGE BTW BEAM 1 AND 2 STA Y= 693 AT MID CARGO DOOR. MID CARGO DOOR WAS REPAIRED PER ER/A 550293-14 REV ORG.
- [SDR DALA2016100307005](https://openairdocs.org/sdr/DALA2016100307005.md): Skin · delaminated · Sep 30, 2016 · N907DE · Doug MD88 · Trailing Edge Flaps
  > DELAMINATED LOWER SKIN ON MID VANE GUIDE OF OUTBD FLAP NEXT TO INBD EDGE, AT RT WING. SERVICEABLE MID VANE GUIDE OUTBD FLAP RT WAS REPLACED PER AMM 27-51-03.
- [SDR DALA2016092906946](https://openairdocs.org/sdr/DALA2016092906946.md): Skin · damaged · Sep 28, 2016 · N907DE · Doug MD88 · Trailing Edge Flaps
  > CP DELAMINATED OUBT GUIDE VANE OUBT FLAP LOWER SKIN INB SECTION AND CLOSE TO LEADING EDGE AT LEFT WING. COMPOSITES. LW. GUIDE VANE REMOVED P/N 5910043-509 S/N DL10 AND GUIDE VANE INSTALLED P/N 5910043-509 S/N 268364. (LP2702347)
- [SDR DALA2016092806916](https://openairdocs.org/sdr/DALA2016092806916.md): Support Fitting · corroded · Sep 27, 2016 · N907DE · Doug MD88 · Fuselage, Landing Gear Attach Fittings
  > CORROSION ON LT MLG RETRACT ACTUATOR SUPPORT FITTING BEARING BORE IN REF AD 5740-01139-04A. REPAIR WAS PERFORMED IAW ER/A 550286-14AD, REV ORIGINAL PERMANENT REPAIR.
- [SDR DALA2016092706887](https://openairdocs.org/sdr/DALA2016092706887.md): Skin · punctured · Sep 26, 2016 · N907DE · Doug MD88 · Trailing Edge Flaps
  > PUNCTURED LOWER SKIN ON OUTER VANE GUIDE OF OTBD FLAP AT RT WING. DUE TO EXCESSIVE DAMAGE ON OUTER VANE GUIDE OF OTBD FLAP AT RT WING WAS REPLACED IAW IPC 27-50-04-01A.
- [SDR DALA2016092606832](https://openairdocs.org/sdr/DALA2016092606832.md): Tab · delaminated · Sep 25, 2016 · N907DE · Doug MD88 · Elevator, Tab Structure
  > INITIAL: DELAMINATED LT CONTROL TAB. ELEVATOR CONTROL TAB LT WAS REPLACED IAW AMM 27-30-03-201.
- [SDR DALA2016092606830](https://openairdocs.org/sdr/DALA2016092606830.md): Stringer · cracked · Sep 25, 2016 · N907DE · Doug MD88 · Fuselage Main, Longeron/Stringer
  > CRACK OF 0.5" ON STR 17LT XCW=12 AT LT CENTER TANK. STRINGER 17LT WAS REPAIRED IAW ER/A 549299-14, REV ORIGINAL. REPAIR APPROVAL IS LIMITED TO 24 MONTHS FROM THE FORM 8100-9 APPROVAL DATE: 16/SEP/16.
- [SDR DALA2016092506829](https://openairdocs.org/sdr/DALA2016092506829.md): Pan · cracked · Sep 24, 2016 · N907DE · Doug MD88 · Cargo/Baggage Doors
  > AWR HIDDEN DISCREPANCY: CRACKED UPPER PAN STA Y=674 AT MID CARGO DOOR. CRACKED UPPER PAN STA Y=674 AT MID CARGO DOOR WAS REPAIRED IAW SRM 52-03D, FIG 8.
- [SDR DALA2016092506828](https://openairdocs.org/sdr/DALA2016092506828.md): Intercostal · cracked · Sep 24, 2016 · N907DE · Doug MD88 · Cargo/Baggage Doors
  > INITIAL: CRACK ON INTERCOSTAL AND ANGLE OF MID CARGO DOOR ON STA PROJECTION Y = 674 BETWEEN BEAM NR 5 AND UPPER EDGE. INTERCOSTAL AND ANGLE OF MID CARGO DOOR ON STA PROJECTION Y = 674 BETWEEN BEAM NR 5 AND UPPER EDGE WERE REPALCED IAW SRM:51-30-1, 51-30-2, 51
- [SDR DALA2016092406824](https://openairdocs.org/sdr/DALA2016092406824.md): Floor Panel · corroded · Sep 23, 2016 · N907DE · Doug MD88 · Fuselage Floor Panel
  > AWR CORROSION ON FLOOR PANEL NR 541E. FLOOR PANEL NR:541E WAS MANUFACTURED BY EXCESSIVE CORROSION IAW AMM 53-20-01-201.
- [SDR DALA2016092206773](https://openairdocs.org/sdr/DALA2016092206773.md): Skin · worn · Sep 21, 2016 · N907DE · Doug MD88 · Trailing Edge Flaps
  > INITIAL: WEAR ON OTBD EDGE UPPER SKIN OF OUTBD VANE GUIDE ON INBD FLAP AT RT WING. RT WING INBD FLAP OTBD GUIDE VANE WAS REPAIRED IAW A/C 9007, CARD 2000-8149-02 AND SRM 57-03D, PARA 11, FIG 11.
- [SDR DALA2016092106758](https://openairdocs.org/sdr/DALA2016092106758.md): Scuff Plate · cracked · Sep 20, 2016 · N907DE · Doug MD88 · Fuselage Miscellaneous Structure
  > CRACKED AND ELONGATED AND HOLES ON SCUFF PLATE, PN 5936070-29 AT MID CARGO. SCUFF PLATE WAS REPAIRED IAW ER/A 491023-14MA, REV A.
- [SDR DALA2016092106756](https://openairdocs.org/sdr/DALA2016092106756.md): Frame · cracked · Sep 20, 2016 · N907DE · Doug MD88 · Fuselage Main, Frame
  > INITIAL: CRACK ON FRAME STA Y=1510 BETWEEN 10 AND 11 O`CLOCK POSITION AT AFT ACCESSORY COMPARTMENT. FRAME ON STA Y=1510 WAS REPLACED IAW SRM 51-30-2.
- [SDR DALA2016092106754](https://openairdocs.org/sdr/DALA2016092106754.md): Skin · cracked · Sep 20, 2016 · N907DE · Doug MD88 · Rudder, Plate/Skin
  > CRACK ON LT RUDDER SKIN AT STA ZR=16 53" TO T/E. DAMAGE ON RUDDER SKIN AT STA ZR=16.53" TO T/E WAS REPAIRED BY SRM 51-70- 1AD, PARA 13 AND JIC CARD 2000-8149-03.
- [SDR DALA2016092006735](https://openairdocs.org/sdr/DALA2016092006735.md): Stringer · cracked · Sep 20, 2016 · N907DE · Doug MD88 · Fuselage Main, Longeron/Stringer
  > CRACK ON STR STA Y= 1463 BETWEEN 10 AND 11 O`CLOCK POSITION AT AFT ACCESSORY COMPARTMENT. STR AT STA Y= 1463 BETWEEN 10 AND 11 CLOCK POSITION WAS REPLACED IAW SRM 51-30-5 AND DWG 9911839, REV DP.
- [SDR DALA2016092006734](https://openairdocs.org/sdr/DALA2016092006734.md): Doubler · worn · Sep 19, 2016 · N907DE · Doug MD88 · Trailing Edge Flaps
  > INITIAL: CM WORN UPPER PREVIOUS DOUBLER REPAIR ON OUTBD GUIDE VANE INBD FLAP OUTBD SECTION AT LT WING. LT WING INBD FLAP OTBD GUIDE VANE WAS REPAIRED IAW A/C 9007 CARD 2000-8149-01, JOB 000-0014 AND SRM 57-03D, PARA 11, FIGURE 11.
- [SDR DALA2016092006732](https://openairdocs.org/sdr/DALA2016092006732.md): Seat Track · corroded · Sep 19, 2016 · N907DE · Doug MD88 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON RT SEAT TRACK FIRST OFFICIAL STA Y 120 TO Y 140 X- 28 AT, CP. RT SEAT TRACK FIRST OFFICIAL STA, Y 120 TO Y 140 X-28 AT WAS REPLACED IAW SRM 51-30-1 AND DWG 9957871, REV V.
- [SDR DALA2016110408282](https://openairdocs.org/sdr/DALA2016110408282.md): Support · corroded · Sep 18, 2016 · N907DE · Doug MD88 · Fuselage Miscellaneous Structure
  > CORROSION ON CEILING SUPPORT ON STA Y= 1231 BTW X=17 LT TO X= 34 LT, STA Y= 1309 BTW X=35 LT TO 35 RT, BTW STA Y= 1231 TO 1309 X= 17 LT, BTW STA Y=1250 TO 1309 X=0 AT AFT CARGO COMPARTMENT. CORROSION WAS REMOVED PER SRM 51-10-3 PAR 26 AND SUPPORTS WERE REPLAC
- [SDR DALA2016091906706](https://openairdocs.org/sdr/DALA2016091906706.md): Intercostal · corroded · Sep 18, 2016 · N907DE · Doug MD88 · Fuselage Miscellaneous Structure
  > INITIAL: CORROSION ON INTERCOSTAL BETWEEN LONGERON 28 LT TO 27 LT AND STA Y= 769 TO Y= 788 AT MID CARGO. INTERCOSTAL WAS REPLACED IAW SRM 51-30-5 AND DWG 9915554, REV J.
- [SDR DALA2016091906705](https://openairdocs.org/sdr/DALA2016091906705.md): Frame · cracked · Sep 18, 2016 · N907DE · Doug MD88 · Fuselage Main, Frame
  > INITIAL: CRACKS 3 EAS ON FRAME STA Y= 1510 LOWER. RT SIDE AT AFT ACCESSORY COMPARTMENT CAT FRAME WAS REPLACED IAW SRM 51-30-2 AND DWG 9911843, REV AC.
- [SDR DALA2016091806703](https://openairdocs.org/sdr/DALA2016091806703.md): Doubler · worn · Sep 17, 2016 · N907DE · Doug MD88 · Cargo/Baggage Doors
  > WEAR ON FWD AND AFT PRODUCTION DOUBLERS AT FWD CARGO COMPARTMENT DOOR SKIN LOWER SECTION. DOUBLERS WERE REPLACED IAW SRM 51-30-2 AND ERA 486624-14, MA REV ORIGINAL.
- [SDR DALA2016091806702](https://openairdocs.org/sdr/DALA2016091806702.md): Pan · cracked · Sep 17, 2016 · N907DE · Doug MD88 · Cargo/Baggage Doors
  > AWR HIDDEN DISCREPANCY: CRACKED PAN JUST ON SEATING AREA OF STOP FITTING PROJECTION BEAM 4, FWD SIDE, AT FWD CARGO DOOR. CRACK ON PAN JUST ON SEATING AREA OF STOP FITTING PROJECTION BEAM 4, FWD SIDE, WAS REPAIRED IAW SRM 52-05-D, FIG 50.
- [SDR DALA2016091606692](https://openairdocs.org/sdr/DALA2016091606692.md): Cargo Track · corroded · Sep 15, 2016 · N907DE · Doug MD88 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON LEFT CARGO TRACK UPPER & LOWER SURFACE BETWEEN BS 1022 AND 1221. THE CARGO TRACK WAS REPLACED IAW SRM 51-30-1,51-30-2 AND DWG 5936660 REV:BZ.
- [SDR DALA2016091606691](https://openairdocs.org/sdr/DALA2016091606691.md): Skin · damaged · Sep 15, 2016 · N907DE · Doug MD88 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN FWD OF C2 DOOR BS 636, DAMAGE WAS BLENDED OUT AND EVALUATED. REWORKED AREAS WERE TREATED AND PAINTED IAW SRM 51-10-3 PARAGRAPH 14 AND 21.
- [SDR DALA2016091606689](https://openairdocs.org/sdr/DALA2016091606689.md): Cargo Track · corroded · Sep 15, 2016 · N907DE · Doug MD88 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON LEFT CARGO TRACK DOWN FROM BS 1222 TO 1322 IN AFT CARGO BAY. THE CARGO TRACK WAS REPLACED IAW SRM 51-30-2, 51-30-5 AND DWG 5936660 REV BZ.
- [SDR DALA2016091606688](https://openairdocs.org/sdr/DALA2016091606688.md): Cargo Track · corroded · Sep 15, 2016 · N907DE · Doug MD88 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON RIGHT CARGO TRACK UPPER & LOWER SURFACE BETWEEN BS 1022 AND 1155 IN AFT CARGO COMPARTMENT. THE CARGO TRACK WAS REPLACED IAW SRM 51-30-1, 51-30-5 AND DWG:5936660 REV BZ.
- [SDR DALA2016091606687](https://openairdocs.org/sdr/DALA2016091606687.md): Angle · corroded · Sep 15, 2016 · N907DE · Doug MD88 · Fuselage Main, Bulkhead
  > CORROSION ON AFT PRESSURE BULKHEAD ANGLE BETWEEN LONGERONS 28L TO 28R IN AFT CARGO BAY. ANGLE WAS REPLACED IAW SRM 51-30-02,51-30-05 AND DWG 9915561 REV CG.

Next page: https://openairdocs.org/deregistered/N907DE-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 = 'N907DE' AND deregistration_id = 'N907DE-2022-11-29'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N907DE-2022-11-29/reports

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