# Service difficulty reports: N947ML, cancelled Oct 31, 2000

A list on [N947ML, cancelled Oct 31, 2000](https://openairdocs.org/deregistered/N947ML-2000-10-31.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 2 · 80 reports

- [SDR GTIA000142](https://openairdocs.org/sdr/GTIA000142.md): Light · inoperative · Mar 18, 2000 · N947ML · Doug DC932 · Emergency Lighting
  > ACY - FLT 812 - ONE FORWARD EMERGENCY TRACK LIGHT INOPERATIVE. DEFERRED TO DMI 81030-1 MEL 33-24, CAT C, PLACARDS INSTALLED. REPLACED FORWARD EMERGENCY TRACK LIGHT SOCKET. OPS CHECK GOOD IAW MM 33-53-0. THIS CLEARS DMI 81030-1. PLACARD REMOVED. (M)
- [SDR GTIA9901159](https://openairdocs.org/sdr/GTIA9901159.md): Wire · broken · Oct 14, 1999 · N947ML · Doug DC932 · Light System Wiring
  > MLB - DURING DAILY, FOUND EMERGENCY FLOOR LIGHTS INOPERATIVE. REPAIRED BROKEN WIRE AND REPLACED BULB AND LENSE AND ROW 4. OPERATION CHECK NORMAL IAW 33-53-0. (M)
- [SDR GTIA9900054](https://openairdocs.org/sdr/GTIA9900054.md): Light · inoperative · Apr 3, 1999 · N947ML · Doug DC932 · Emergency Lighting
  > DTW - EMERGENCY EXIT LIGHT INOPERATIVE. MAIN ENTRY DOOR WAY. REMOVED AND REPLACED LIGHT ASSEMBLY. FUNCTIONAL CHECK GOOD DC-9 MM CHAP 33-50-0. (M)
- [SDR GTIA9800079](https://openairdocs.org/sdr/GTIA9800079.md): Slide · loose · Jul 1, 1998 · N947ML · Doug DC932 · Emergency Equipment
  > MAIN CABIN DOOR ESCAPE SLIDE FELL OUT DUE TO JET BLAST. REINSTALLED ESCAPE SLIDE AS REQUIRED. NO DEFECTS NOTED AT THIS TIME IAW DC9 MM 25-61-0. ALL ACCOMPLISHED. (M)
- [SDR GTIA9800051](https://openairdocs.org/sdr/GTIA9800051.md): Prox Switch · dirty · Apr 23, 1998 · N947ML · Doug DC932 · Landing Gear Position and Warning
  > LRD - FLT 902 - LANDING GEAR EXTENSION WAS NORMAL. ABOUT 700 FEET ABOVE THE RUNWAY, RT MAIN GEAR RED UNSAFE LIGHT CAME ON FOR 1-2 SECONDS, EVER 5-10 SECONDS. WENT AROUND BUT THE LEFT GEAR DOWN. UNSAFE INDICATIONS STOPPED. USED QRH PROCEDURES, RECYCLED GEAR
- [SDR GTIA9700407](https://openairdocs.org/sdr/GTIA9700407.md): Lights · missing · Nov 22, 1997 · N947ML · Doug DC932 · Emergency Lighting
  > DTW - FLT 626 - MISSING 2 LIGHTS IN THE EMERGENCY TRACK LIGHTING (RED ONES) BY FWD EXITS. REINSTALLED LENS AND LAMPS IN EMERGENCY TRACK LIGHTING. OPS CHECK GOOD. (M)
- [SDR GTIA9700401](https://openairdocs.org/sdr/GTIA9700401.md): Bulb · missing · Nov 17, 1997 · N947ML · Doug DC932 · Emergency Lighting
  > FLL - FLT 411 - MOST FORWARD EMERGENCY FLOOR LIGHT IS INOPERATIVE AND 4TH LIGHT FROM FORWARD IS MISSING. INSTALLED BULB, OPS CHECK GOOD. (M)
- [SDR GTIA9700398](https://openairdocs.org/sdr/GTIA9700398.md): Bulbs · missing · Nov 3, 1997 · N947ML · Doug DC932 · Emergency Lighting
  > PIE - FORWARD SECTION OF RED FLOOR TRACK LIGHTING MISSING 2 LENSES AND LAMPS. REPLACED 2 RED LENSES AND LAMPS IN FORWARD SECTION OF FLOOR TRACK LIGHTING. OPS CHECKS OK PER DC-9 MM CHAPTER 33. (M)
- [SDR GTIA9700346](https://openairdocs.org/sdr/GTIA9700346.md): Bulb · missing · Jul 21, 1997 · N947ML · Doug DC932 · Emergency Lighting
  > DTW - FLT 640 - FORWARD FIRST ROW OF RED EMERGENCY EXITS LIGHTS HAS BULB MISSING. INSTALLED NEW BULB, OPS CHECK GOOD. (M)
- [SDR GTIA970338](https://openairdocs.org/sdr/GTIA970338.md): Relay · sticking · Jul 7, 1997 · N947ML · Doug DC932 · AC Power Distribution System
  > PIT - FLT 202 - APPARENTLY THE RIGHT A/C BUS HAS AN APU RELAY STICKING WHICH WILL NOT ALLOW ANY OTHER POWER SOURCE TO POWER THE RIGHT A/C BUS. THIS OCCURS EVEN WITH THE APU SHUT DOWN. RESET CROSS-TIE RELAY. APU GEN SYSTEM INOP. TRANSFERRED DMI LOG NR 00712
- [SDR GTIA9700319](https://openairdocs.org/sdr/GTIA9700319.md): Battery · discharged · Jun 26, 1997 · N947ML · Doug DC932 · Emergency Lighting
  > DTW - ON DAILY INSPECTION, FOUND TRACK LIGHTING NOT TESTING PROPERLY. REPLACED TRACK LIGHTING EMERGENCY BATTERY ASSEMBLY. SYSTEM TESTED NORMAL IAW DC-9 MM 33-50-00. (M)
- [SDR GTIA9700309](https://openairdocs.org/sdr/GTIA9700309.md): Altimeter · failed · Jun 4, 1997 · N947ML · Doug DC932 · Altimeter, Barometric/Encoder
  > ACY - FLT 178 - BARO ALTIMETER IS READING 150 FEET AT FIELD ELEVATION OF 76 FEET ON CAPTAIN'S SIDE. REMOVED AND REPLACED CAPTAIN'S ALTIMETER PER MM 34-10-6. CLEARS DMI NR 00594. PER GMM CHAPTER 4, PAGE 8.1, REV 25, ITEM 2.B.1. PITOT/STATIC LEAK CHECK TO BE
- [SDR GTIA9700306](https://openairdocs.org/sdr/GTIA9700306.md): Tire · failed · May 31, 1997 · N947ML · Doug DC932 · Tire
  > MYR - FLT 111 - LEFT OTBD TIRE BLEW OUT ON EXITING RUNWAY. NORMAL BRAKING, BUT BRAKES APPEARED UNUSUALLY SENSITIVE. EXITING RUNWAY SPEED ABOUT 30 KNOTS ON HIGH SPEED TAXI-WAY MYR. NR 2 MLG TIRE DUE CHANGE, DUE TO NR 1 TIRE BLOW OUT PER GMM CHAP 4, PG 7.5.
- [SDR GTIA9700300](https://openairdocs.org/sdr/GTIA9700300.md): Elev Pwr Light · malfunctioned · May 26, 1997 · N947ML · Doug DC932 · Elevator Control System
  > BOS - FLT 243 - ON TAXI OUT, ELEV POWER LIGHT CAME ON PRIOR TO TEST. DURING TEST, LIGHT ON, THEN OFF, NORMAL IND. WITHIN 30 SECONDS LIGHT REAPPEARED VERY DIM, BUT INCREASED IN INTENSITY TO FULL BRIGHT. SHUT DOWN LEFT ENGINE, NORMAL IND RESTARTED LEFT, NORMA
- [SDR GTIA9700294](https://openairdocs.org/sdr/GTIA9700294.md): Warning Light · illuminated · May 26, 1997 · N947ML · Doug DC932 · Door Warning System
  > MYR - FLT 1706 - STAIRWAY DOOR LIGHT CAME ON APPROXIMATELY 1 HOUR INTO FLIGHT, BUT DID EXTINGUISH PRIOR TO LANDING. (2ND OCCURRENCE). TRANSFERRED TO DMI LOG, DMI NR 00574, FORWARD AIRSTAIR DOOR LGIHT PER MEL 33-17 (CAT C). FORWARD AIRSTAIR VERIFIED CLOSED A
- [SDR GTIA9700293](https://openairdocs.org/sdr/GTIA9700293.md): Lens Cover · out of position · May 26, 1997 · N947ML · Doug DC932 · Emergency Lighting
  > MYR - FLT 243 - STAIRWAY DOOR LIGHT CAME ON APROXIMATELY 1 HOUR INTO FLIGHT. FOUND BOTTOM STAIR LIGHT LENS INTERFERRING WITH DOOR CLOSURE. SECURED LENS COVER. STAIRS AND DOOR OPS CHECKS GOOD. (X)
- [SDR GTIA9700292](https://openairdocs.org/sdr/GTIA9700292.md): Bulb · failed · May 24, 1997 · N947ML · Doug DC932 · Emergency Lighting
  > ACY - FLT 210 - THIRD LIGHT AFT ON FLOOR LIGHTING INOPERABLE. REPLACED BULB. OPS CHECK GOOD IAW 33-50-0. (X)
- [SDR GTIA9700305](https://openairdocs.org/sdr/GTIA9700305.md): Mic Jack · shorted · May 13, 1997 · N947ML · Doug DC932 · Audio Integrating System
  > MYR - FLT 182 - LOSS OF BOTH RADIOS WHILE SITTING ON END OF RUNWAY FOR TAKEOFF. AFTER TAXI BACK TO RAMP AND DURING ENGINE SHUT DOWN, RADIOS STARTED WORKING NORMALLY. INSPECTED COMM SYSTEMS AND FOUND FAULTY MIC JACK (SHORTED INTERNALLY) AT OB'S POSITION. REM
- [SDR GTIA9700273](https://openairdocs.org/sdr/GTIA9700273.md): Locking Mech · lack of lube · Apr 6, 1997 · N947ML · Doug DC932 · Fixed Inner Doors
  > ACY - FLT 196 - COCKPIT DOOR WILL NOT LOCK DURING TAXI OUT. LUBED AND CLEANED LOCKING MECHANISM. OPS CHECK GOOD OK FOR FURTHER FLIGHT. (M)
- [SDR GTIA9700266](https://openairdocs.org/sdr/GTIA9700266.md): Annunciator Pnl · malfunctioned · Apr 1, 1997 · N947ML · Doug DC932 · Central Warning
  > DTW - FLT 428 - STAIRWAY DOOR LIGHT CAME ON DURING FLIGHT. TROUBLESHOT SYSTEM, FOUND INTERMITTENT ANNUNCIATOR LIGHT. REMOVED AND REPLACED ANNUNCIATOR PANEL. SYSTEM OPS CHECK GOOD IAW DC9 MM CH 52-70-0. (M)
- [SDR GTIA9700265](https://openairdocs.org/sdr/GTIA9700265.md): Warning Light · illuminated · Mar 28, 1997 · N947ML · Doug DC932 · Door Warning System
  > DTW - FLT 428 - IN CRUISE, STAIRWAY DOOR LIGHT ILLUMINATED. THERE WAS NOT ANY ADDITIONAL NOISE BY CABIN DOOR OR ANY PRESSURIZATION CHANGES. CYCLED AIRSTAIR SEVERAL TIMES AND LIGHT WENT OUT WITH EVERY CYCLE. OPS CHECK GOOD. (M)
- [SDR GTIA9700263](https://openairdocs.org/sdr/GTIA9700263.md): Hinge · broken · Mar 27, 1997 · N947ML · Doug DC932 · Passenger/Crew Doors
  > DTW - FLT 428 - AFT ENTRY DOOR, LOWER HINGE BROKEN. REMOVED AND REPLACED LOWER HINGE, AFT ENTRY DOOR, OVBD HINGE HALF ONLY IAW DC-9 MM 52-20. (M)
- [SDR GTIA9700234](https://openairdocs.org/sdr/GTIA9700234.md): Air Data Comp · malfunctioned · Mar 14, 1997 · N947ML · Doug DC932 · Air Data Computer
  > YIP - REF DME NR 00127 (MRR NR 97-01-27-003/GTIA9700147). AUTOPILOT PORPOISES IN ALL FLIGHT MODES (CLIMB, CRUISE, DESCENT, STABILIZED FLIGHT). FUNCTIONAL CHECK PERFORMED IAW DC-9 MM 22-10-0. READ WIRING TO PITCH CHANNELS. REMOVED AND REPLACED AIR DATA COMP
- [SDR GTIA9700188](https://openairdocs.org/sdr/GTIA9700188.md): Aileron Trim · binding · Mar 9, 1997 · N947ML · Doug DC932 · Aileron Tab Control System
  > DTW - AILERON TRIM BINDING AND POSITION INDICATOR WILL NOT CENTER. FOUND SPIRAL DRIVE PLATE ON AILERON TRIM INDICATOR TO BE BINDING AND EXCESSIVELY WORN. REPLACED IAW DC-9 MM 27-10-7. OPS CHECK GOOD. (X)
- [SDR GTIA9700182](https://openairdocs.org/sdr/GTIA9700182.md): Wire · loose · Mar 7, 1997 · N947ML · Doug DC932 · Landing Gear System Wiring
  > ACY - FLT 825 - NOSE GEAR GREEN LIGHT STAYS ON WITH LANDING GEAR UP. UPLATCH CHECKS OK. LANDING GEAR INDICATIONS NORMAL IN DOWN POSITION. NOSE GEAR RED LIGHT OUT IN UP POSITION AS IT SHOULD BE. REMOVED LANDING GEAR LIGHT CLUSTER. FOUND WIRE GROUNDING OUT
- [SDR GTIA9700239](https://openairdocs.org/sdr/GTIA9700239.md): Autopilot · malfunctioned · Mar 5, 1997 · N947ML · Doug DC932 · Autopilot System
  > ACY - FLT 700 - AUTOPILOT PORPOISES PLUS OR MINUS 2,000 PER MINUTE VERTICALLY IN CLIMB, CRUISE, DESCENT, IN-FLIGHT. UNUSABLE. ENTER IN DMI LOG NR 00230 PER MEL 22-1 CAT 'C' DUE 3-15-97 ID NR 120. (MRR NR GTIA9700229). REMOVED AND REPLACED AVG COMPUTERS IAW
- [SDR GTIA9700211](https://openairdocs.org/sdr/GTIA9700211.md): Skin · damaged · Feb 28, 1997 · N947ML · Doug DC932 · Fuselage Main, Plate/Skin
  > YIP - REPAIR FUSELAGE SKIN DAMAGE AT FS 465-500, LONGERON 23R AND 24R PER SPIRIT EA 5330-97-003. FABRICATED REPAIR IAW SPIRIT EA 5330-97-003. REPAIRED FUSELAGE SKIN FS AT 465-500 PER SPIRIT EA 5330-97-003. (M)
- [SDR GTIA9700204](https://openairdocs.org/sdr/GTIA9700204.md): Skin · corroded · Feb 28, 1997 · N947ML · Doug DC932 · Fuselage Main, Plate/Skin
  > YIP - REPAIR FUSELAGE SKIN BETWEEN FS 270 - FS 370, LONGERONS 23R TO 26R PER SPIRIT EA 5330-97-004. REPAIRED FUSELAGE SKIN AT FS 270-370, LONGERONS 23R - 26R PER SPIRIT EA 5330-97-004. (X)
- [SDR GTIA9700210](https://openairdocs.org/sdr/GTIA9700210.md): Panel · delaminated · Feb 27, 1997 · N947ML · Doug DC932 · Fuselage Main, Plate/Skin
  > YIP - LEFT ADF PANEL DELAMINATED. MANUFACTURED FIXTURE TO TRANSFER HOLES. DRILLED HOLES AND COUNTERSUNK AS REQUIRED. TEST FIT AND TRIMMED ALL EDGES OF EXCESS MATERIAL. PAINTED ANTENNA. INSTALLED USING PROPER SCREWS. (X)
- [SDR GTIA9700205](https://openairdocs.org/sdr/GTIA9700205.md): Sill · corroded · Feb 26, 1997 · N947ML · Doug DC932 · Fuselage Miscellaneous Structure
  > YIP - FORWARD CARGO DOOR SILL LOWER - SPOTS OF CORROSION AROUND SCREW HOLES. REMOVED CORROSION AND TREATED IAW DC-9 SRM 51-10-3. (X)
- [SDR GTIA9700201](https://openairdocs.org/sdr/GTIA9700201.md): Doubler · damaged · Feb 26, 1997 · N947ML · Doug DC932 · Cargo/Baggage Doors
  > YIP - EXTERNAL REPAIR DOUBLER ON LOWER EDGE OF CARGO DOOR, FS 928 NEEDS TO BE REMOVED. REMOVED OLD DOUBLER AND INSTALLED NEW REPAIR DOUBLER PER EA 5330-97-005. (X)
- [SDR GTIA9700198](https://openairdocs.org/sdr/GTIA9700198.md): Doubler · loose rivets · Feb 26, 1997 · N947ML · Doug DC932 · Fuselage Miscellaneous Structure
  > YIP - REMOVE RIVETS, INSTALL HI-LOCKS IN REPAIR DOUBLER FS 937 BETWEEN LONGERONS 23L AND 24L. REMOVED RIVETS IN REPAIR DOUBLER, INSTALLED HI-LOCKS IN DOUBLER PER EA 5330-97-006. (X)
- [SDR GTIA9700206](https://openairdocs.org/sdr/GTIA9700206.md): Panel · delaminated · Feb 24, 1997 · N947ML · Doug DC932 · Fuselage Main, Plate/Skin
  > YIP - RIGHT ADF PANEL DELAMINATED. MANUFACTURED FIXTURE TO TRANSFER HOLES. DRILLED HOLES AND COUNTERSUNK AS REQUIRED. TEST FIT AND TRIMMED ALL EDGES OF EXCESS MATERIAL. PAINTED ANTENNA. INSTALLED USING PROPER HARDWARE. (X)
- [SDR GTIA9700202](https://openairdocs.org/sdr/GTIA9700202.md): Mount · damaged · Feb 23, 1997 · N947ML · Doug DC932 · Engine Mount Section
  > YIP - LEFT NACELLE, ENGINE MOUNT: UPPER AFT VIBRATION ABSORBER ASSY LOOSE, STEM BENT. ALSO, SUSPECT THREADS DAMAGED. REMOVED AND REPLACED ABSORBER IAW DC-9 MM 71-20-3. THREADS IN PYLON YOKE ATTACH BOLT GOOD. (X)
- [SDR GTIA9700190](https://openairdocs.org/sdr/GTIA9700190.md): Oxygen Line · leaking · Feb 23, 1997 · N947ML · Doug DC932 · Passenger Oxygen System
  > YIP - DURING FUNCTIONAL CHECK OF OXYGEN MASK DEPLOYMENT TEST, FOUND DEFECTIVE LEAKING LINE AT SUPPLY MANIFOLD (L13 OVERHEAD PANEL LOCATION). REQUIRES LEAK CHECK. SERVICEABLE LINE INSTALLED IAW DC-9 MM 35-20-2. NO LEAKS NOTED. (X)
- [SDR GTIA9700189](https://openairdocs.org/sdr/GTIA9700189.md): Splice · cracked · Feb 21, 1997 · N947ML · Doug DC932 · Fuselage Miscellaneous Structure
  > YIP - FORWARD BELLY COMPARTMENT, NR 22 LONGERON CORRODED AND SPLICE PLATE CRACKED AT FS 229. REPAIRED LONGERON AT FS 229 PER DC-9 SRM 53-02. (X)
- [SDR GTIA9700224](https://openairdocs.org/sdr/GTIA9700224.md): Control Cable · frayed · Feb 20, 1997 · N947ML · Doug DC932 · Aileron Control System
  > YIP - LEFT WING - AILERON CABLE FRAYED NEAR FAIR LEAD AT APPROXIMATELY STA XRS 353. MANUFACTURED AND INSTALLED CABLE, TENSIONED AND SAFTIED IAW DC-9 MM CHAPTER 27-10-0 PAGES 9 AND 10, AND CABLE TENSION CHART. (X)
- [SDR GTIA9700216](https://openairdocs.org/sdr/GTIA9700216.md): Skin · damaged · Feb 19, 1997 · N947ML · Doug DC932 · Trailing Edge Flaps
  > YIP - REPAIR ON RIGHT FLAP TRAILING EDGE AT APPROXIMATELY STATION XRS 138-156 BE REMOVED AND REPLACED WITH NEW. REMOVED AND REPLACED RIGHT FLAP TRAILING EDGE WITH NEW PART IAW DC9 SRM 57-03 PAGE 11. (M)
- [SDR GTIA9700197](https://openairdocs.org/sdr/GTIA9700197.md): Doubler · damaged · Feb 19, 1997 · N947ML · Doug DC932 · Fuselage Miscellaneous Structure
  > YIP - EXTERNAL REPAIR DOUBLER FS 351 BETWEEN LONGERONS 18R AND 20R REQUIRES REWORK. REWORKED REPAIR DOUBLER AT RIGHT FUS 351 TO C/W REQUIREMENTS OF DC-9 SRM 53-04 FIG 12B (INSTALLATION OF FINGER DOUBLER AND PROPER FASTENERS). (X)
- [SDR GTIA9700200](https://openairdocs.org/sdr/GTIA9700200.md): Bracket · cracked · Feb 18, 1997 · N947ML · Doug DC932 · Trailing Edge Flaps
  > YIP - LEFT FLAP, INBOARD ATTACH BRACKET CRACKED. (CONFIRMED WITH EDDY CURRENT.) REMOVED AND REPLACED LEFT INBOARD ATTACH BRACKET WITH NEW BRACKET IAW DC-9 MM 20-16-0 PAGE 207. (X)
- [SDR GTIA9700227](https://openairdocs.org/sdr/GTIA9700227.md): Trap Panel · cracked · Feb 17, 1997 · N947ML · Doug DC932 · Fuselage Miscellaneous Structure
  > YIP - ULTRASONIC INDICATION FROM FORWARD MOST END OF UPPER ATTACH FLANGE THROUGH FIRST ATTACH HOLE TO FORWARD END OF SECOND ATTACH HOLE OF LEFT TRAP PANEL (APPROXIMATE LENGTH, 2 INCHES). REMOVED OUTBOARD PORTION OF CRACKED FLANGE AND CORROSION IAW DC-9 SRM 57
- [SDR GTIA9700199](https://openairdocs.org/sdr/GTIA9700199.md): Fairing · corroded · Feb 17, 1997 · N947ML · Doug DC932 · Horizontal Stabilizer Structure
  > YIP - LEFT HORIZONTAL STABILIZER LOWER SCRAPPER FAIRING: INTERIOR BOX CHANNEL HAS SURFACE CORROSION ALONG ATTACH EDGES. REMOVED MINOR SURFACE CORROSION IAW DC-9 SRM 51-10-3. (X)
- [SDR GTIA9700195](https://openairdocs.org/sdr/GTIA9700195.md): Rivet · failed · Feb 14, 1997 · N947ML · Doug DC932 · Horizontal Stabilizer Structure
  > YIP - LEFT UPPER HORIZONTAL STABILIZER FAIRING - POPPED RIVET AT AFT ATTACH AND AFT CDCC AREA CRACKED. REPAIRED CRACK AND INSTALLED EXTERNAL DOUBLER AND FILLER PER DC-9 SRM 55-01 PAGE 7, 51-30-2 AND USING MATERIAL AS PRESCRIBED IN DC-9 SRM 55-10-0, PAGE 11, F
- [SDR GTIA9700192](https://openairdocs.org/sdr/GTIA9700192.md): Clip · broken · Feb 14, 1997 · N947ML · Doug DC932 · Fuselage Miscellaneous Structure
  > YIP - FS 148 CIRCUMFERENTIAL APPROXIMATELY 12 INCHES LEFT OF CENTER OVERHEAD, BROKEN ANGLE CLIP. MANUFACTURED REPAIR ANGLE IAW DC-9 SRM 51-10-1. INSTALLED ANGLE IAW DC-9 SRM 51-30-1. (X)
- [SDR GTIA9700223](https://openairdocs.org/sdr/GTIA9700223.md): Bute Door · damaged · Feb 13, 1997 · N947ML · Doug DC932 · Wing, Plate/Skin
  > YIP - LEFT WING, CENTER BUTE DOOR INBOARD EDGE, SKIN DAMAGED. INSTALLED NEW DOOR ASSEMBLY IAW MM 57-20-3. (X)
- [SDR GTIA9700196](https://openairdocs.org/sdr/GTIA9700196.md): Skin · damaged · Feb 12, 1997 · N947ML · Doug DC932 · Cargo/Baggage Doors
  > YIP - AFT CARGO DOOR, DOOR HANDLE CUT OUT - SKIN DAMAGED. REPAIRED SKIN DAMAGE IAW DC-9 SRM 52-05, FIG 30. (X)
- [SDR GTIA9700222](https://openairdocs.org/sdr/GTIA9700222.md): Skin · corroded · Feb 11, 1997 · N947ML · Doug DC932 · Wing, Plate/Skin
  > YIP - LEFT WING UPPER SURFACE EVIDENCE OF CORROSION IN 'NO STEP' AREA BETWEEN STA XRS 383-581 (TRAILING EDGE). CLEANED SURFACE CORROSION, TREATED AREA, AND PAINTED IAW DC-9 SRM 51-10-3. (X)
- [SDR GTIA9700217](https://openairdocs.org/sdr/GTIA9700217.md): Skin · corroded · Feb 11, 1997 · N947ML · Doug DC932 · Wing, Plate/Skin
  > YIP - RIGHT WING UPPER SURFACE TRAILING EDE HAS EVIDENCE OF CORROSION AT STA XRS 383-531 'NO STEP' AREA. BLENDED OUT CORROSION AND TREATED (REF: DC-9 SRM 51-10-3) IN NO STEP AREA STA 383-531. PREPPED, PRIMED, AND PAINTED RIGHT WING UPPER SURFACE TRAILING ED
- [SDR GTIA9700214](https://openairdocs.org/sdr/GTIA9700214.md): Angle · corroded · Feb 11, 1997 · N947ML · Doug DC932 · Fuselage Miscellaneous Structure
  > YIP - FORWARD CARGO COMPARTMENT O/H STATION 370 SPOTS OF CORROSION ON LINER SUPPORT ANGLE FROM 0 TO 16 INCH LEFT OF CENTER. REMOVED CORROSION AND TREATED IAW DC-9 SRM 51-10-3. PAINTED IAW 51-10-3B. (M)
- [SDR GTIA9700213](https://openairdocs.org/sdr/GTIA9700213.md): Mount · corroded · Feb 11, 1997 · N947ML · Doug DC932 · Cargo/Baggage Doors
  > YIP - FORWARD CARGO DOOR AFT BUNGEE MOUNT BRACKET SPOTS OF CORROSION AT BOLT HOLES. REMOVED AND TREATED CORROSION FORWARD CARGO DOOR AFT BUNGEE MOUNT BRACKET IAW DC-9 SRM 51-10-3. (M)

Next page: https://openairdocs.org/deregistered/N947ML-2000-10-31/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 = 'N947ML' AND deregistration_id = 'N947ML-2000-10-31'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N947ML-2000-10-31/reports

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.