# Service difficulty reports: N934ML, cancelled Aug 1, 2001

A list on [N934ML, cancelled Aug 1, 2001](https://openairdocs.org/deregistered/N934ML-2001-08-01.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 · 180 reports

- [SDR GTIA010209](https://openairdocs.org/sdr/GTIA010209.md): Angle · cracked · Apr 18, 2001 · N934ML · Doug DC931 · Service Doors
  > FTW - FOUND R-1 DOOR BETWEEN BEAM NR 2 AND NR 3 SKIN ANGLE HAS CRACK. (M)
- [SDR GTIA010221](https://openairdocs.org/sdr/GTIA010221.md): Drive Link · cracked · Apr 10, 2001 · N934ML · Doug DC931 · Drag Control System
  > FOUND RIGHT INBOARD SPOILER DRIVE LINK CRACKED. REMOVED DRIVE LINK IAW DC-9 MM 27-61-2 OK TO INSTALL DRIVE LINK. INSTALLED DRIVE LINK IAW MM DC-9 27-61-2. (M)
- [SDR GTIA010223](https://openairdocs.org/sdr/GTIA010223.md): Flap · chafed · Apr 2, 2001 · N934ML · Doug DC931 · Trailing Edge Flaps
  > FTW - LEFT FLAP INBOARD TRAILING EDGE CHAFING. REMOVED LEFT FLAP INBOARD TRAILING EDGE. (M)
- [SDR GTIA010222](https://openairdocs.org/sdr/GTIA010222.md): Cowling · cracked · Mar 19, 2001 · N934ML · Doug DC931 · Engine Cowling System
  > FTW - NR 2 ENGINE PYLON FIXED COWL CRACKED 3 PLACES. REMOVED EDGE MEMBER FROM ANGLE IAW DC-9 SRM 34-02. (M)
- [SDR GTIA010001](https://openairdocs.org/sdr/GTIA010001.md): Wire · loose · Jan 1, 2001 · N934ML · Doug DC931 · Light System Wiring
  > DTW - FLT 58 - WHEN TURNING ON THE NOSE LIGHT TO BRIGHT POSITION, SPARKS WERE VISIBLE COMING FROM THE SWITCH AREA FOLLOWED BY LIGHT SMOKE. TIGHTENED LOOSE WIRE IAW DC-9 MM 33-41. OPS CHECK GOOD. (M)
- [SDR GTIA000343](https://openairdocs.org/sdr/GTIA000343.md): Connector · disconnected · Dec 16, 2000 · N934ML · Doug DC931 · Emergency Lighting
  > ACY - FOUND L1 EMERGENCY EXIT IDENTIFIER INOPERATIVE. FOUND CANNON PLUG DISCONNECTED. RECONNECTED CANNON PLUG OPS CHECK GOOD IAW MM DC9 33-50-00. (M)
- [SDR GTIA000342](https://openairdocs.org/sdr/GTIA000342.md): Wire · exposed · Dec 1, 2000 · N934ML · Doug DC931 · Light System Wiring
  > DISCREPANCY: EMERG. FLOOR TRACK LIGHTING AT ROWS 14,17,18,23&15 HAVE EXPOSED WIRING. CORRECTIVE ACTION: READJUSTED AND SECURED EMERGENCY TRACK LIGHTING. OPS CHECKED GOOD IAW DC-9 M/M 33-50-0
- [SDR GTIA000314](https://openairdocs.org/sdr/GTIA000314.md): Light · inoperative · Nov 3, 2000 · N934ML · Doug DC931 · Emergency Lighting
  > FLL - FOUND EMERGENCY PATH LIGHT OUT AT EMERGENCY EXIT, RED LIGHT. REPLACED LAMP, OPS CHECKED OK. REF MM 33-51-00. (M)
- [SDR GTIA000280](https://openairdocs.org/sdr/GTIA000280.md): Light · inoperative · Aug 28, 2000 · N934ML · Doug DC931 · Emergency Lighting
  > LGB- FLT 903 - AISLE PATH LIGHT OUT OF BOX IN FORWARD ENTRANCE. SECURED EMERGENCY FLOOR TRACK IT. COVER IAW DC-9 MM 33-50. OPS CHECK GOOD. (M)
- [SDR GTIA000196](https://openairdocs.org/sdr/GTIA000196.md): Light · misinstalled · May 10, 2000 · N934ML · Doug DC931 · Emergency Lighting
  > DTW - FOUND EMERGENCY FLOOR TRACK LIGHTING STRIP AT 1 EF IS HELD DOWN BY CARGO PIT TAPE. RESECURED TRACK IAW 33-50-00, NO DEFECTS NOTED. (M)
- [SDR GTIA000154](https://openairdocs.org/sdr/GTIA000154.md): Light · missing · Apr 1, 2000 · N934ML · Doug DC931 · Emergency Lighting
  > FLL - AISLE FLOOR TRACK LIGHTING MISSING ONE RED LENS AT ROW 14 DEF. ASSIGNED DMI 91308-2 PER MEL 33-24 CAT C, DUE 4/11/00. (M)
- [SDR GTIA000136](https://openairdocs.org/sdr/GTIA000136.md): Lens · missing · Mar 15, 2000 · N934ML · Doug DC931 · Emergency Lighting
  > DTW - EMERGENCY FLOOR TRACK LIGHTING AT ROW 19 MISSING LENS COVER AND LAMP. RELAMPED AND INSTALLED LENS COVER. OPS CHECK NORMAL IAW MM 33-51-1. (M)
- [SDR GTIA000015](https://openairdocs.org/sdr/GTIA000015.md): Lens · missing · Jan 10, 2000 · N934ML · Doug DC931 · Emergency Lighting
  > TPA - EMERGENCY FLOOR PATH LIGHTING FOUND TO HAVE ONE RED LENS COVER AND BULB MISSING AFT OF AIRCRAFT. REPLACED MISSING BULB AND RES LENS COVER TO EMERGENCY EGRESS LIGHTING. OPERATIONAL CHECK PERFORMED FUNCTIONS. (M)
- [SDR GTIA000014](https://openairdocs.org/sdr/GTIA000014.md): Light · malfunctioned · Jan 9, 2000 · N934ML · Doug DC931 · Emergency Lighting
  > ISP - FLT 432 - EMERGENCY AISLE LIGHTING CAME ON IN FLIGHT AND WOULD NOT GO OUT. OPS CHECK SEVERAL TIMES ON GROUND NO DISCREPANCIES NOTED. (M)
- [SDR GTIA000011](https://openairdocs.org/sdr/GTIA000011.md): Light · loose · Jan 6, 2000 · N934ML · Doug DC931 · Emergency Lighting
  > DTW - FORWARD EMERGENCY TRACK LIGHTING STRIP TEMPORARILY SECURED WITH SPEED TAPE. REPLACED EMERGENCY LIGHTING STRIP AND INSTALLED THRESHOLD PLATE IAW DC-9 SRM 51-30-2. (M)
- [SDR GTIA0000001](https://openairdocs.org/sdr/GTIA0000001.md): Placard · missing · Jan 2, 2000 · N934ML · Doug DC931 · Placards and Markings
  > DTW - FLT 91 - SOME OF THE SEATS THE PLACARDS 'LIFE VEST UNDER SEAT' ARE MISSING. REPLACED MISSING PLACARDS IAW DC9 MM 11-41-00. (M)
- [SDR GTIA9901234](https://openairdocs.org/sdr/GTIA9901234.md): Wire · damaged · Dec 25, 1999 · N934ML · Doug DC931 · Light System Wiring
  > MCO - FLT 92 - AFT ENTRY EMERGENCY 'EXIT' SIGN ON LEFT SIDE WALL INOPERATIVE. REPAIRED GROUND WIRE AT AFT ENTRY OVERHEAD. PANEL AND OPS CHECKED GOOD PER MM CHECK 33-50-00. (M)
- [SDR GTIA9901213](https://openairdocs.org/sdr/GTIA9901213.md): Battery · discharged · Dec 1, 1999 · N934ML · Doug DC931 · Emergency Lighting
  > DTW - FLT 880 - AFT EMERGENCY EXIT (OVER WING) SIGNS (UPPER) WILL NOT LIGHT LEFT AND RIGHT. REPLACED BATTERIES IN EMERGENCY POWER PACK AT BS-25. OPS CHECK GOOD. REF: MD 80 MM 33-53-00. (X)
- [SDR GTIA9901212](https://openairdocs.org/sdr/GTIA9901212.md): Splice · failed · Nov 26, 1999 · N934ML · Doug DC931 · Emergency Lighting
  > ACY - FLT 880 - AISLE PATH LIGHTING FORWARD OF ROW 12 IS INOPERABLE. REPAIRED SPLICE, OPS CHECK GOOD. IAW MM 33-21-0. (X)
- [SDR GTIA9901092](https://openairdocs.org/sdr/GTIA9901092.md): Bulb · failed · Aug 25, 1999 · N934ML · Doug DC931 · Emergency Lighting
  > DTW - LEFT UPPER EMERGENCY LIGHT IS OUT. RELAMPED, OPERATIONS CHECKS GOOD AT THIS TIME. (M)
- [SDR GTIA9901090](https://openairdocs.org/sdr/GTIA9901090.md): Light · inoperative · Aug 25, 1999 · N934ML · Doug DC931 · Emergency Lighting
  > DTW - CENTER OVERHEAD LIGHT EMERGENCY LIGHT BROKEN. CENTER OVERHEAD PANEL ASSEMBLY REMOVED. REPLACED BULB AND SOCKET TO CENTER OVERHEAD LIGHT (EMERGENCY ASSEMBLY. REINSTALLED PANEL ASSEMBLY. SYSTEM AROUND CHECKED GOOD ALL IAW DC-9 MM SECTION 33-00-0. (M)
- [SDR GTIA9901089](https://openairdocs.org/sdr/GTIA9901089.md): Power Supply · inoperative · Aug 25, 1999 · N934ML · Doug DC931 · Emergency Lighting
  > DTW - ROW TWO EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED BATTERY POWER SUPPLY. OPERATION CHECKS GOOD IAW DC-9 MM 33-50-00. (M)
- [SDR GTIA9901081](https://openairdocs.org/sdr/GTIA9901081.md): Battery Pack · discharged · Aug 17, 1999 · N934ML · Doug DC931 · Emergency Lighting
  > MYR - FLT 619 - LEFT NACELLE EMERGENCY LIGHT WILL NOT ILLUMINATE. TRANSFERRED TO DEFERRED MAINTENANCE ITEM NR 320. REMOVED AND REPLACED LEFT EMERGENCY NACELLE BATTERY PACK IAW MM CHAPTER 33-53-0. OPERATION CHECKS GOOD. (M)
- [SDR GTIA9901091](https://openairdocs.org/sdr/GTIA9901091.md): Light · inoperative · Aug 5, 1999 · N934ML · Doug DC931 · Emergency Lighting
  > DTW - AFT OVERHEAD EMERGENCY LIGHT ASSEMBLY BROKEN. REPLACED BULB AND SOCKET TO AFT OVERHEAD EMERGENCY LIGHT ASSEMBLY. SYSTEM CHECKED GOOD ALL IAW DC9 MM SECTION 33-00-00. (M)
- [SDR GTIA9901067](https://openairdocs.org/sdr/GTIA9901067.md): Light · inoperable · Aug 3, 1999 · N934ML · Doug DC931 · Emergency Lighting
  > AFT CABIN DOOR EMERGENCY LIGHT (HAND HELD) INOPERATIVE. REMOVED AND REPLACED AFT CABIN DOOR EMERGENCY LIGHT ASSY IAW DC-9 MM 33-50-00. (X)
- [SDR GTIA9901025](https://openairdocs.org/sdr/GTIA9901025.md): Frame · cracked · Jul 28, 1999 · N934ML · Doug DC931 · Fuselage Main, Frame
  > MHV - PASSENGER CABIN INTERNAL LEFT SIDE AT STA 560 AFT SIDE OF FRAME CRACKED APROXIMATELY 2 INCHES ABOVE FLOOR LINE. REMOVED FITTING FOR INSPECTION. REPAIRED DAMAGED AREA IAW DC9 SRM 51-01 AND SRM 53-01. ALODINED AND PRIMED IAW DC9 SRM 51-10-6. REINSTALLE
- [SDR GTIA9901021](https://openairdocs.org/sdr/GTIA9901021.md): Spring · broken · Jul 28, 1999 · N934ML · Doug DC931 · Galley Doors
  > MHV - FORWARD GALLEY DOOR ROLLER ASSY FOR THE DOOR BAYONET SPRING IS BROKEN ALLOWING THE ROLLER ASSY TO FLOAT WHEN THE DOOR IS BEING CLOSED. PERMITS BAYONET TO JAM BEHIND THE ROLLER ASSY. REMOVED AND REINSTALLED BROKEN SPRING WITH NEW ONE AW DC9 MM 52-41-0, P
- [SDR GTIA9900985](https://openairdocs.org/sdr/GTIA9900985.md): Batery Charger · inoperative · Jul 8, 1999 · N934ML · Doug DC931 · Emergency Lighting
  > DTW - CABIN, A NUMBER OF OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY CHARGER STAND, CHECK GOOD IAW MM 33-50-00. (M)
- [SDR GTIA9900984](https://openairdocs.org/sdr/GTIA9900984.md): Bulb · failed · Jul 8, 1999 · N934ML · Doug DC931 · Emergency Lighting
  > DTW - AFT VENTRAL STAIRS SIDEWALL LIGHTS HAVE INOPERATIVE EMERGENCY LIGHT PORTION. RELAMPED CHECK GOOD AIW 33-50-00. (M)
- [SDR GTIA9900983](https://openairdocs.org/sdr/GTIA9900983.md): Light · inoperative · Jul 8, 1999 · N934ML · Doug DC931 · Emergency Lighting
  > AFT ACCESSORIES COMPARTMENT CAT WALK MISSING EMERGENCY LIGHT LENSE AND BULB. REPLACED EMERGENCY LIGHT LENSE AND BULB IAW DC-9 MM 33-51-00. (M)
- [SDR GTIA9901019](https://openairdocs.org/sdr/GTIA9901019.md): Panel · misaligned · May 24, 1999 · N934ML · Doug DC931 · Vertical Stabilizer, Plate/Skin
  > MHV - REPLACEMENT VERTICAL UPPER CENTER PANEL PN 9911940-403 ATTACH HOLES DO NOT ALIGN WITH AIRCRAFT STRUCTURE. FABED IN REF TO DC9 SRM 51-10 MANUFACTURED FOLLOWING ITEMS. 2 EACH CHANNELS 1 EA RT. 1 EACH LT. 2 INCH Z-CLIPS, 1 EACH RT, 1 EACH LT. 2 BULKHEA
- [SDR GTIA9901018](https://openairdocs.org/sdr/GTIA9901018.md): Panel · cracked · May 24, 1999 · N934ML · Doug DC931 · Vertical Stabilizer, Plate/Skin
  > MHV - VERTICAL STABILIZER CENTER PANEL UPPER, PN 9911940-403, HAS CRACK RT AFT SIDE APPROXIMATELY 8 INCHES LONG. CENTER PANEL REPAIR AND INSTALLATION TO BE ACCOMPLISHED ON A092-A03-N065. (X)
- [SDR GTIA9901011](https://openairdocs.org/sdr/GTIA9901011.md): Panel · misaligned · May 24, 1999 · N934ML · Doug DC931 · Vertical Stabilizer, Plate/Skin
  > MHV - VERTICAL CENTER PANEL UPPER P/N 9911940-403 WHICH WAS REPLACED ON W/C NO062 HAS ATTACHING HOLES MISALIGNING WITH MATING HOLES ON VERT STRUT. PER ENG DWG NR 9909001 INSTALLATION COMPLETE PARTS FAB ON W/C A092-B10-N067 BRACKETS, CHANNELS, STRAPS ALL INSTA
- [SDR GTIA9901006](https://openairdocs.org/sdr/GTIA9901006.md): Structure · damaged · May 24, 1999 · N934ML · Doug DC931 · Horizontal Stabilizer Structure
  > MHV - REMOVAL OF HORIZONTAL STABILIZER IS REQUIRED TO REPLACE WITH SERVICEABLE UNIT. REMOVED AND REPLACED HORIZONTAL STAB ASSY PER DC9 MM 55-10-0 PAGE 202. HORIZ STABILIZER ADJUSTMENT AND TEST C/W PER DC9 MM 55-10-0 PAGE 501 HORIZ STAB ACCESS PANELS WILL BE
- [SDR GTIA9901026](https://openairdocs.org/sdr/GTIA9901026.md): Floor · cracked · May 22, 1999 · N934ML · Doug DC931 · Fuselage Floor Panel
  > MHV - CABIN CENTER RIGHT FLOOR PANEL STA 598 TO STA 639 HAS (5 EACH) CRACKS (3 EACH AT FASTENER HOLES AND TWO BELOW FASTENER HOLES). REPAIRED CRACKS INSTALLED DOUBLERS IAW SRM DC9 53-05 FAB DOUBLERS IAW SRM DC9 53-05 ALODINED AND PRIMED IAW SRM DC9 51-10-3.
- [SDR GTIA9901016](https://openairdocs.org/sdr/GTIA9901016.md): Floorbeam · mismanufactured · May 22, 1999 · N934ML · Doug DC931 · Fuselage Main, Floor Beam
  > MHV - BS 996 FLOORBEAM UPPER CAP ANGLE FROM LBL 12 TO EOP AT LBL 52 REQUIRES NEW SECTION TO ACCOMMODATE LT AFT LAV FLOOR STRUCTURE MOD. C/W ENGINEERING DWG NR 53-99197-2. ALODINED AND PRIMED. (X)
- [SDR GTIA9901015](https://openairdocs.org/sdr/GTIA9901015.md): Support · cracked · May 22, 1999 · N934ML · Doug DC931 · Fuselage Miscellaneous Structure
  > MHV - CABIN CENTER LT FLOOR PANEL STA 579 TO STA 680 (BOTTOM OF FLOOR PANEL SUPPORT 2 AND 4 HAS CRACKS AND PUNCTURE HOLES). REMOVED SUPPORTS 2 AND 4 IAW SRM DC9 53-05 AND REPLACED SUPPORTS 2 AND 4 IAW SRM DC9 53-05. (X)
- [SDR GTIA9901013](https://openairdocs.org/sdr/GTIA9901013.md): Stringer · misdrilled · May 22, 1999 · N934ML · Doug DC931 · Fuselage Main, Longeron/Stringer
  > MHV - PASSENGER CABIN INTERNAL STATION 550 TO 570 STRINGER L-17 THERE ARE APPROX 25 HOLES WITH SHORT C/C SPACING S/B.600 IAW SRM 53-02 FIG 18 SH 6 ARE.48-.58 REF NR A092-S03-W084. REMOVED AND REPLACED SKIN AND LONGERON SECTIONS FROM STATION 531 TO STATION 5
- [SDR GTIA9901010](https://openairdocs.org/sdr/GTIA9901010.md): Floor · worn · May 22, 1999 · N934ML · Doug DC931 · Fuselage Floor Panel
  > MHV - LEFT CABIN FLOOR PANEL STATION 669 TO 775 SKIN AROUND NUMEROUS SCREW HOLES TO THIN. RESKINNED FLOOR PANEL IAW SRM DC9 53-20 AND 53-05, FABRICATED SKIN PANEL ALODINED AND PRIMED. (M)
- [SDR GTIA9901009](https://openairdocs.org/sdr/GTIA9901009.md): Shear Tie · cracked · May 22, 1999 · N934ML · Doug DC931 · Fuselage Miscellaneous Structure
  > REMOVED B/S REPAIR RT FUSE CRACK IN SHEAR TIE APPRON STATION 940 BETWEEN STRINGER 15/16. FABRICATED ANGLE DOUBLER PER DC9 IAW SRM 51-10-2 PAGE 1 FIG 2 PER SAMPLE SUPPLIED. (M)
- [SDR GTIA9901004](https://openairdocs.org/sdr/GTIA9901004.md): Intercostal · cracked · May 22, 1999 · N934ML · Doug DC931 · Fuselage Miscellaneous Structure
  > MHV - PASSENGER CABIN INTERNAL STATION 484 LONGERON R-6 INTERCOSTAL CRACKED. REMOVED CRACK INTERCOSTAL AS REQUIRED TO FACILITATE FABRICATION OF REPLACEMENT PAR REF W/O A092-B03-W131 COPY ATTACHED INSTALLED REPLACEMENT AS REQUIRED PER DC9 SRM 51-30-5 AND 51-10
- [SDR GTIA9900101](https://openairdocs.org/sdr/GTIA9900101.md): Intercostal · cracked · May 22, 1999 · N934ML · Doug DC931 · Fuselage Miscellaneous Structure
  > MHV - PASSENGER CABIN STATION 484 LONGERON R6 INTERCOSTAL CRACKED. FABRICATED REPLACEMENT ITEM REF DC9 SRM 51-10 HEAT TREAT NOT REQUIRED ISSUED TO AIRCRAFT FOR FIT AND INSTALL ON W/O A092B03W106. (M)
- [SDR GTIA9900100](https://openairdocs.org/sdr/GTIA9900100.md): Intercostal · cracked · May 22, 1999 · N934ML · Doug DC931 · Fuselage Miscellaneous Structure
  > MHV - PASSENGER CABIN INTERNAL STATION 484 LONGERON R-6 INTERCOSTAL CRACKED. REMOVED CRACK INTERCOSTAL AS REQUIRED TO FACILITATE FABRICATION OF REPLACEMENT PAR REF W/O A092-B03-W131 COPY ATTACHED INSTALLED REPLACEMENT AS REQUIRED PER DC9 SRM 51-30-5 AND 51-10
- [SDR GTIA9901024](https://openairdocs.org/sdr/GTIA9901024.md): Longeron · cracked · May 21, 1999 · N934ML · Doug DC931 · Fuselage Main, Longeron/Stringer
  > MHV - PASSENGER CABIN INTERNAL STA 560 LONGERON L-17 HAS A CRACK. HOLES WERE MIS-DRILLED. REPAIR WILL BE ACCOMPLISHED ON W/C NR A092-S39-W132. W132 - REMOVED AND REPLACED SKIN AND LONGERON SECTIONS FROM STA 531 TO STA 588, PRODUCTION SPLICE PER ENGINEERING
- [SDR GTIA9901023](https://openairdocs.org/sdr/GTIA9901023.md): Stringer · cracked · May 21, 1999 · N934ML · Doug DC931 · Fuselage Main, Longeron/Stringer
  > MHV - BS 207 LT, STR 13 WEB IS CRACKED. RECEIVED VERIFICATION OF REPAIR MAT'L ON P.O. NR 80319. TRIMMED CRACKED MEMBER IAW DC9 SRM 53-01. ALODINED AND PRIMED IAW DC9 SRM 51-10-6. INSTALLED REPAIR FILLER AND DOUBLER IAW DC9 SRM 53-01 AND SRM 51-30-2. (X)
- [SDR GTIA9901022](https://openairdocs.org/sdr/GTIA9901022.md): Web · cracked · May 21, 1999 · N934ML · Doug DC931 · Fuselage Miscellaneous Structure
  > MHV - CABIN STA 617 RBL 48, CRACK IN WEB. STOP DRILLED CRACK. FABRICATED REPAIR DOUBLER. ALODINED AND PRIMED AND INSTALLED DOUBLER IAW SRM 53-01 FIG 2 (SHEET 3). (X)
- [SDR GTIA9901017](https://openairdocs.org/sdr/GTIA9901017.md): Stiffener · cracked · May 19, 1999 · N934ML · Doug DC931 · Rudder Structure
  > MHV - RUDDER RIB STIFFENER IS CRACKED, PN 5910256. FABBED NEW STIFFENER AND HEAT TREATED PER AMS-H 6080 AND DC9 SRM 51-10-2 PURCHASE AYA. PART REPAIR PART NOT REQUIRED. (X)
- [SDR GTIA9901008](https://openairdocs.org/sdr/GTIA9901008.md): Skin · cracked · May 19, 1999 · N934ML · Doug DC931 · Rudder, Plate/Skin
  > MHV - THERE ARE 2 CRACKS ON THE RUDDER RIGHT SIDE AT RIB NR 6 AND RIB NR 8. REMOVED AND REPLACED RUDDER AND SKIN AND 1 STIFFENER IAW DC9 SRM 55-03 AND S/B 55-23R6 CNI AND AD87-08-03 W/B TO BE ACCOMPLISHED ON WO A092A03 N061. PAINT TO BE ACCOMPLISHED ON W/O A
- [SDR GTIA9901014](https://openairdocs.org/sdr/GTIA9901014.md): Panel · worn · May 18, 1999 · N934ML · Doug DC931 · Horizontal Stabilizer, Plate/Skin
  > MHV - HORIZONTAL STABILIZER CENTER SECTION PANEL NR 3804A AFT AND LOWER SECTION WORN TO KNIFE EDGE. FABRICATED REPAIR DOUBLERS REF DC9 SRM 5503. HEATED TREATED AND AGE HARDENED PER AMS H 6088. ASSEMBLED AND ISSUED FOR INSTALLATION ON WO A092107022. (X)
- [SDR GTIA9901007](https://openairdocs.org/sdr/GTIA9901007.md): Skin · cracked · May 18, 1999 · N934ML · Doug DC931 · Horizontal Stabilizer, Plate/Skin
  > MHV - HORIZONTAL STABILIZER CENTER SECTION UPPER RIGHT PANEL NR 3806A CRACKED AT AFT UPPER AREA ALSO WORN TO KNIFE EDGE. FABRICATED DOUBLER AND FILLER TO COVER DAMAGED PANEL, INSTALLED PER DC9 IAW SRM 55-03-0 PAGE 28 VIEW F ALODINE AND PRIMED PER DC9 IAW SRM

Next page: https://openairdocs.org/deregistered/N934ML-2001-08-01/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 = 'N934ML' AND deregistration_id = 'N934ML-2001-08-01'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N934ML-2001-08-01/reports

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