# Service difficulty reports: N906AT

A list on [N906AT](https://openairdocs.org/aircraft/N906AT.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 · 160 reports

- [SDR DALA2026090304980](https://openairdocs.org/sdr/DALA2026090304980.md): Flap · no discrepancy · Sep 3, 2026 · N906AT · Boeing 717200 · Wing, Plate/Skin
  > EVIDENCE OF RUBBING ON LEADING EDGE OF LEFT INBOARD FLAP LOCATED JUST ABOVE MAIN LANDING GEAR. PAINT SHOWING BARE METAL IN THAT AREA, INSPECTED LT INBD FLAP AND FOUND NO EVIDENCE OF RUBBING OR CHAFING PER B717 AMM 27-50. (9116531) (AIRCRAFT GROUNDED).
- [SDR DALA2026090304979](https://openairdocs.org/sdr/DALA2026090304979.md): Flap · no discrepancy · Sep 2, 2026 · N906AT · Boeing 717200 · Wing, Plate/Skin
  > POTENTIAL RUB DAMAGE ON UNDERSIDE OF THE LEFT WING FLAP. LOCATED JUST ABOVE MAIN LANDING GEAR, INSPECTED LT INBD FLAP AND FOUND NO EVIDENCE OF RUBBING OR CHAFING IAW AMM 27-50. (9116528) (AIRCRAFT GROUNDED).
- [SDR DALA2026082504810](https://openairdocs.org/sdr/DALA2026082504810.md): Girt Bar · unsecure · Aug 24, 2026 · N906AT · Boeing 717200 · Emergency Equipment
  > L1 DOOR SLIDE APPEARS TO BE BROKEN, RESECURED GIRT BAR IAW AMM 52-11. (9092292) (AIRCRAFT GROUNDED).
- [SDR DALA2026071304130](https://openairdocs.org/sdr/DALA2026071304130.md): O-Ring · leaking · Jul 10, 2026 · N906AT · Boeing 717200 · Engine Fuel Distribution
  > NR 1 ENGINE FUEL LEAK ON WALK AROUND STRONG FUEL ODOR ON APU AIR. R & R O-RING IAW AIPC 73-12-05-22. (8831910) (AIRCRAFT GROUNDED)
- [SDR DALA2026011600378](https://openairdocs.org/sdr/DALA2026011600378.md): Windshield · cracked · Jan 10, 2026 · N906AT · Boeing 717200 · Flight Compartment Windows
  > DIVERTED TO BNA FOR CAPT. WINDSHIELD OUTER PANE CRACKED. MAINTENANCE CLEANED, INSPECTED, PRESSURIZED AND RETURNED TO SERVICE WITH NO FAULTS DETECTED.(7498293)
- [SDR DALA2026010900242](https://openairdocs.org/sdr/DALA2026010900242.md): Handle · broken · Jan 5, 2026 · N906AT · Boeing 717200 · Cargo/Baggage Doors
  > AFT CARGO DOOR HANDLE IS BROKEN OFF & MISSING. INSTALLED AFT CARGO DOOR HANDLE REF B717 CMM 52-30-2. OPS CHECK GOOD. (7498261)
- [SDR DALA2024111410956](https://openairdocs.org/sdr/DALA2024111410956.md): Battery Pack · no test · Nov 14, 2024 · N906AT · Boeing 717200 · Emergency Lighting
  > THE EMERGENCY EXIT SIGNS ARE INOPERATIVE AT STATION 180, STATION 247, AND STATION 706. MAINTENANCE REPLACED THE EMERGENCY BATTERY PACKS B5-235, B5-259, AND B5-120 PER B717 AMM 33-51. OPERATION CHECK WAS NORMAL. (LP #5423934)
- [SDR DALA2024081608213](https://openairdocs.org/sdr/DALA2024081608213.md): Battery Pack · inoperative · Aug 16, 2024 · N906AT · Boeing 717200 · Emergency Lighting
  > OVERWING DOOR EMERGENCY LIGHTS ARE INOPERATIVE. T/S OVERWING DOOR EMERGENCY LIGHTS PER B717 FIM 33-50-00 810-801. REPLACED THE EMERGENCY LIGHT BATTERY PACK AT LOCATION B5-230 PER B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. AIRCRAFT OK FOR SERVICE. (LP #6010188
- [SDR DALA2024062106299](https://openairdocs.org/sdr/DALA2024062106299.md): Latch · loose · Jun 19, 2024 · N906AT · Boeing 717200 · Landing Gear Doors
  > SHIP 9582 -GEAR/DE- DURING THE FINAL APPROACH FOR LANDING THE AIRCRAFT INDICATED A "GEAR UNSAFE" CONDITION FOR ALL 3 GEAR POSITIONS. AN EMERGENCY WAS DECLARED WITH ATC, THE QRH WAS COMPLIED WITH, AND THE ALTERNATE GEAR EXTENSION PROCEDURES WERE UTILIZED, WHICH
- [SDR DALA2024042304672](https://openairdocs.org/sdr/DALA2024042304672.md): Relay · faulted · Apr 22, 2024 · N906AT · Boeing 717200 · Brake Anti-Skid Section
  > SHIP 9582 -MISC/DE- THE FLIGHT CREW RECEIVED AN "ANTI-SKID FAIL" MESSAGE DURING LANDING GEAR EXTENSION ON APPROACH INTO MSP. AN EMERGENCY WAS DECLARED BY THE CREW. THE MESSAGE EXTINGUISHED BEFORE LANDING. CORRECTIVE ACTION: AFTER LANDING, ALL BRAKE TEMPERATURE
- [SDR DALA2023121110134](https://openairdocs.org/sdr/DALA2023121110134.md): Unknown · unknown · Dec 10, 2023 · N906AT · Boeing 717200 · Doors
  > CORROSION ON INTERNAL SKIN AT STAIRWAY DOOR. SUMMARY OF NRC 00568: CORROSION LEVEL 2. STAIRWAY DOOR ASSEMBLY WAS REPLACED PER B717-200 AMM 52-63-01 420-801. (LP #0104041)
- [SDR DALA2023120609977](https://openairdocs.org/sdr/DALA2023120609977.md): Unknown · unknown · Dec 5, 2023 · N906AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CRACK PAN ON FWD AND AFT UPPER CORNERS AT (L1) PASSENGER ENTRANCE DOOR INTERNAL STRUCTURE. SUMMARY OF NRC 00176: PAN OF FWD UPPER CORNER AT (L1) PASSENGER ENTRANCE DOOR INTERNAL STRUCTURE WAS REPLACED PER B-717-200 SRM 51-41-02-0G AND 51-41-04-0G PROCEDURE GEN
- [SDR DALA2023112809760](https://openairdocs.org/sdr/DALA2023112809760.md): Unknown · unknown · Nov 27, 2023 · N906AT · Boeing 717200 · Passenger/Crew Doors
  > CRACK ON PASSENGER ENTRANCE DOOR NO.1 BEAM BTW STA Y 160-165 APPROX INTERNAL STRUCTURE (L1). SUMMARY OF NRC 00687: PASSENGER ENTRANCE DOOR NO.1 BEAM BTW STA Y 160-165 APPROX INTERNAL STRUCTURE WAS REPAIRED PER B717-200 SRM 52-10-02-2R PROCEDURE 7 REPAIR 7. (LP
- [SDR DALA2023112809753](https://openairdocs.org/sdr/DALA2023112809753.md): Unknown · unknown · Nov 26, 2023 · N906AT · Boeing 717200 · Fuselage Main, Frame
  > CORROSION ON PREVIOUS SPLICE REPAIR ON FRAME STA 974 BTW LONG 30 AND 27 LH IN REF NRC 00216. SUMMARY OF NRC 00685: CORROSION LEVEL 2. PREVIOUS SPLICE REPAIR ON FRAME STA 974 BTW LONG 30 AND 27 LH WERE REPLACED AND INSTALLED PER B717-200 SRM 53-20-07-2R PROCEDU
- [SDR DALA2023112809765](https://openairdocs.org/sdr/DALA2023112809765.md): Unknown · unknown · Nov 25, 2023 · N906AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > DIMENSIONAL MEASUREMENTS WERE FOUND OUT OF LIMITS ON SECTION OF WING BOX UPPER SKIN BTW STA Y=750 AND X=19 TO X=59 AT LH MLG/ WHEEL WELL (SM) AFTER CORROSION REMOVAL. SUMMARY OF NRC 00640: CORROSION LEVEL 2. DIMENSIONAL MEASUREMENTS WERE FOUND OUT OF LIMITS ON
- [SDR DALA2023112709724](https://openairdocs.org/sdr/DALA2023112709724.md): Unknown · unknown · Nov 25, 2023 · N906AT · Boeing 717200 · Fuselage, Seat/Cargo Attach Fittings
  > CORRODED LH TIE TRACK BTW STA Y=902/1022 AT AFT CARGO COMPARTMENT AREA WAS REWORKED AND IS OUT OF LIMITS. SUMMARY OF NRC 00683: CORROSION LEVEL 2. LH TIE TRACK BTW STA Y=902/1022 AT AFT CARGO COMPARTMENT WAS REPLACED AND INSTALLED PER B717 SRM 51-41-01-0G AND
- [SDR DALA2023112209652](https://openairdocs.org/sdr/DALA2023112209652.md): Unknown · unknown · Nov 21, 2023 · N906AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CRACKS ON CORNER FWD ON SCUFF PLATE AT AFT CARGO. SUMMARY OF NRC 00002: SCUFF PLATE AT AFT CARGO WAS REPAIRED PER ER/A 542149-14TR REV B. SECTION I, PERMAMENT REPAIR. ASSOCIATED ER/A 14-542149 ADDED FOR AC 9582. (LP #0075763)
- [SDR DALA2023112109572](https://openairdocs.org/sdr/DALA2023112109572.md): Unknown · unknown · Nov 20, 2023 · N906AT · Boeing 717200 · Fuselage Internal Mounting Structure
  > CORROSION ON FRAME CLIP STA Y=946 AND BTW LONG 29R/28L AT AFT CARGO COMPARTMENT, WAS FOUND TO BE OUT OF LIMITS. SUMMARY OF NRC 00636: CORROSION LEVEL 2. FRAME CLIP WAS REPLACED PER DWG 9919603 REV CC AND B717 SRM 51-41-02-0G AND 51-41-05-0G. (LP #0074154)
- [SDR DALA2023112009520](https://openairdocs.org/sdr/DALA2023112009520.md): Unknown · unknown · Nov 17, 2023 · N906AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > CRACK ON UPPER AFT CORNER OF FUSSELAGE SKIN AT LH SLIDING WINDOW CUTOUT IN REF TO NRC 00651. SUMMARY OF NRC 00663: UPPER AFT CORNER OF FUSSELAGE SKIN AT LH SLIDING WINDOW CUTOUT WAS REPAIRED PER B717-200 SRM 56-10-02-2R PROCEDURE 1 REPAIR 1. (LP #0069478)
- [SDR DALA2023111509407](https://openairdocs.org/sdr/DALA2023111509407.md): Unknown · unknown · Nov 15, 2023 · N906AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION ON WEB BTW STA Y=954/994 AND BTW LONG=28R/29R AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00220: CORROSION LEVEL 2. WEB BTW STA Y=954/994 AND BTW LONG=28R/29R AT AFT CARGO COMPARTMENT WAS REPLACED AND INSTALLED PER B717-200 SRM 51-41-02-0G AND 51-41-05-
- [SDR DALA2023111409351](https://openairdocs.org/sdr/DALA2023111409351.md): Unknown · unknown · Nov 13, 2023 · N906AT · Boeing 717200 · Fuselage Main, Longeron/Stringer
  > CRACK ON LONGERON 2RH STA Y=1133 AT AFT ACCESSORY. SUMMARY OF NRC 00660: CRACK ON LONGERON 2RH STA Y=1133 AT AFT ACCESSORY WAS REPAIRED PER B717-200 SRM 53-00-05-2R PROCEDURE 2, REPAIR 2. (LP #0063433)
- [SDR DALA2023111409349](https://openairdocs.org/sdr/DALA2023111409349.md): Unknown · unknown · Nov 13, 2023 · N906AT · Boeing 717200 · Fuselage Main, Longeron/Stringer
  > CRACK ON LONGERON 2RH STA Y=1133 AT AFT ACCESSORY. SUMMARY OF NRC 00660: CRACK ON LONGERON 2RH STA Y=1133 AT AFT ACCESSORY WAS REPAIRED PER B717-200 SRM 53-00-05-2R PROCEDURE 2, REPAIR 2. (LP #0063330)
- [SDR DALA2023111309303](https://openairdocs.org/sdr/DALA2023111309303.md): Unknown · unknown · Nov 10, 2023 · N906AT · Boeing 717200 · Fuselage Main, Structure
  > CORROSION ON DOOR JAMB AFT CARGO COMPARTMENT STA Y 960 TO STA Y 986 C2. SUMMARY OF NRC 00040: CORROSION LEVEL 2. DOOR JAMB AFT CARGO COMPARTMENT STA Y 960 TO STA Y 986 C2 WAS REPLACED AND INSTALLED PER B717-200 SRM 53-20-15-2R PROCEDURE 7, 51-41-02-0G, AND 51-
- [SDR DALA2023110709161](https://openairdocs.org/sdr/DALA2023110709161.md): Unknown · unknown · Nov 7, 2023 · N906AT · Boeing 717200 · Fuselage Main, Bulkhead
  > CORROSION ON (Y CHORD) FRAME OF BULKHEAD STA Y=1053 AND BTW LONG 28L/28R AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00229: CORROSION LEVEL 2. (Y CHORD) FRAME OF BULKHEAD STA Y=1053 AND BTW LONG 28L/28R AT AFT CARGO COMPARTMENT WAS REPLACED AND INSTALLED PER B717
- [SDR DALA2023110609114](https://openairdocs.org/sdr/DALA2023110609114.md): Unknown · unknown · Nov 4, 2023 · N906AT · Boeing 717200 · Fuselage Main, Bulkhead
  > CORROSION ON AFT PRESSURE BULKHEAD SKIN LOWER AREA STA Y=1053 AND BTW LONGERON 27R/27L AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00428: CORROSION LEVEL 2. AFT PRESSURE BULKHEAD SKIN LOWER AREA STA Y=1053 AND BTW LONGERON 27R/27L AT AFT CARGO COMPARTMENT WAS REP
- [SDR DALA2023110409089](https://openairdocs.org/sdr/DALA2023110409089.md): Unknown · unknown · Nov 3, 2023 · N906AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CRACK ON LOWER SURFACE OF CUSP WEB STA Y 217 TO STA Y237 AND X=56 AT CPAX. SUMMARY OF NRC 00397: CUSP WEB STA Y 217 TO STA Y237 AND X=56 WAS REPAIRED PER B717-200 SRM 53-00-55-2R-4. (LP #0048292)
- [SDR DALA2023110409088](https://openairdocs.org/sdr/DALA2023110409088.md): Unknown · unknown · Nov 3, 2023 · N906AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CRACK ON CUSP WEB BTW STA 651 TO STA 661 AND X=56 AT CPAX. SUMMARY OF NRC 00374: CUSP WEB BTW STA 651 TO STA 661 AND X=56 AT CPAX WAS REPAIRED PER B717-200 SRM 53-00-55 REPAIR 4. (LP #0048006)
- [SDR DALA2023110309045](https://openairdocs.org/sdr/DALA2023110309045.md): Unknown · unknown · Nov 1, 2023 · N906AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION ON FLOOR SUPPORTS STA Y 148 TO STA Y 200 AND X=7 AND STA Y 162 TO STA Y 195 AND X=56 AT PASSENGER CABIN. IN REF NRC 0395. W1. SUMMARY OF NRC 00559: CORROSION LEVEL 2. SUPPORTS STA Y 148 TO STA Y 200 AND X=7 AND STA Y 162 TO STA Y 195 AND X=56 WERE RE
- [SDR DALA2023110309044](https://openairdocs.org/sdr/DALA2023110309044.md): Unknown · unknown · Nov 1, 2023 · N906AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION ON RH CUSP WEBS BTW ON STA Y=470, Y=493, AND Y=526 X=-56 AT PAX CABIN. SUMMARY OF NRC 00566: CORROSION LEVEL 2. RH CUSP WEBS BTW ON STA Y=470, Y=493, AND Y=526 X=-56 AT PAX CABIN. WERE REPAIRED PER B717 SRM-53-00-55-2R PROCEDURE 4 REPAIR 4 AND SRM 51
- [SDR DALA2023110309043](https://openairdocs.org/sdr/DALA2023110309043.md): Unknown · unknown · Nov 1, 2023 · N906AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION ON FLOOR SUPPORT STA 185 TO 194 X=54 AT PASSENGER CABIN. W1. SUMMARY OF NRC 00521: CORROSION LEVEL 2. FLOOR SUPPORT STA 185 TO 194 X=54 AT PASSENGER CABIN WAS MANUFACTURED AND INSTALLED PER DWG 9936534-101 REV BW AND B717-200 SRM 51-41-02-0G AND 51-4
- [SDR DALA2023110108976](https://openairdocs.org/sdr/DALA2023110108976.md): Unknown · unknown · Oct 31, 2023 · N906AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION ON WEB STA Y 185 TO STA Y 200 BTW X=49 TO X=56 AT CPAX (W1). SUMMARY OF NRC 00396: CORROSION LEVEL 2. WEB STA Y 185 TO STA Y 200 BTW X=49 TO X=56 AT CPAX (W1) WAS REPAIRED PER B717-200 SRM 51-70-10-2R-1 FIG 201. (LP #0043371)
- [SDR DALA2023103108932](https://openairdocs.org/sdr/DALA2023103108932.md): Unknown · unknown · Oct 30, 2023 · N906AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION ON FLOOR SUPPORT BTW STA Y 160 TO STA Y 200 AND -X44 AT PASSENGER CABIN IN REF TO NRC 00392. SUMMARY OF NRC 00477: CORROSION LEVEL 2. NEW FLOOR SUPPORT BTW STA Y 160 TO STA Y 200 AND -X44 WAS REPLACED PER B717 SRM 51-41-02-0G, 51-41-05-0G PAR 8, AND
- [SDR DALA2023103108931](https://openairdocs.org/sdr/DALA2023103108931.md): Unknown · unknown · Oct 30, 2023 · N906AT · Boeing 717200 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON RH OUTBD SEAT TRACK REPAIR PLUG BTW STA 984 TO 988 PAX CABIN. SUMMARY OF NRC 00638: CORROSION LEVEL 1. SEAT TRACK REPAIR PLUG WAS REPLACED PER B717-200 SRM-53-20-52-2R PROCEDURE 1 REPAIR 1 AND 51-41-01-0G. (LP #0042043)
- [SDR DALA2023103008877](https://openairdocs.org/sdr/DALA2023103008877.md): Unknown · unknown · Oct 27, 2023 · N906AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > PUNCTURE ON DIAPHGRAM STA Y 155 X=7 AT PAX CABIN IN REF NRC 0395. W1. SUMMARY OF NRC 00561: DIAPHGRAM STA Y 155 X=7 AT PAX CABIN WAS REPAIRED PER B717 SRM 51-70-10-2R-2. (LP #0037357)
- [SDR DALA2020032001944](https://openairdocs.org/sdr/DALA2020032001944.md): Power Supply · defective · Mar 20, 2020 · N906AT · Boeing 717200 · Emergency Lighting
  > THE AFT EXIT LIGHT IS MALFUNCTIONING BLINKING. MAINTENANCE REPLACED THE AFT POWER SUPPLY PER B717 AMM 33-51. OPERATION IS NOW NORMAL. (LP #7217374
- [SDR DALA2020011700374](https://openairdocs.org/sdr/DALA2020011700374.md): Battery · discharged · Jan 16, 2020 · N906AT · Boeing 717200 · Emergency Lighting
  > THE AFT EMERGENCY EXIT SIGN, CAPTAINS SIDE, IS INOPERATIVE. MAINTENANCE FOUND THAT ALL OF THE ASSOCIATED LIGHTS WITH EMERGENCY POWER SUPPLY B5-260 WERE FLASHING IN THE ARMED POSITION. THE BATTERY AND BATTERY POWER SUPPLY WERE REPLACED PER AMM 33-51-03. ALL OPE
- [SDR DALA2019051302990](https://openairdocs.org/sdr/DALA2019051302990.md): Battery · discharged · May 10, 2019 · N906AT · Boeing 717200 · Emergency Lighting
  > THE AFT EXIT AND EMERGENCY LIGHTS IN THE CATWALK ARE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY AND CHARGED IT AT B-5260. LIGHTS NOW CHECK NORMAL PER AMM 33-51. (LP #5664562)
- [SDR DALA2019020400714](https://openairdocs.org/sdr/DALA2019020400714.md): Battery Pack · inoperative · Feb 1, 2019 · N906AT · Boeing 717200 · Emergency Lighting
  > THE TAIL CONE EMERGENCY EXIT LIGHTS ARE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK AND THE CHARGER PER B717 AMM 33-51. CHECK WAS GOOD. (LP #3790932)
- [SDR DALA2018111986673](https://openairdocs.org/sdr/DALA2018111986673.md): Battery Pack · inoperative · Nov 17, 2018 · N906AT · Boeing 717200 · Emergency Lighting
  > THE CAT WALK IN THE TAIL CONE LOWER EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY IN REAR OF AIRCRAFT AND THE CAT WALK EMERGENCY LIGHTS RETURNED TO NORMAL FUNCTION IAW B717 AMM 33-50. (LP #5174986)
- [SDR DALA2018081305059](https://openairdocs.org/sdr/DALA2018081305059.md): Skin · corroded · Aug 8, 2018 · N906AT · Boeing 717200 · Wing, Plate/Skin
  > SURFACE CORROSION FOUND AT THE LT UPPER WING SKIN, STRINGER 5 LWS 343 TO 348.5. THE CORROSION WAS BEYOND THE LIMITS IAW SRM 57-10-01, ALLOWABLE DAMAGE 1.
- [SDR DALA2018080704894](https://openairdocs.org/sdr/DALA2018080704894.md): Frame · cracked · Aug 6, 2018 · N906AT · Boeing 717200 · Fuselage Main, Frame
  > CRACK INDICATION GREATER THAN 0.125 INCH AT THE BS 696 FRAME TAB UPPER RADIUS. REPLACED THE FRAME IAW AMDS 5310-01436-03B.
- [SDR DALA2018080604893](https://openairdocs.org/sdr/DALA2018080604893.md): Slide · loose · Aug 4, 2018 · N906AT · Boeing 717200 · Escape Slide
  > TAILCONE SLIDE PACK WAS LOOSE AND UNRAVELED. INSTALLED A NEW TAILCONE SLIDE IAW AMM 25-61-02, AND AMDS CARD 5352-4002.
- [SDR DALA2018032601904](https://openairdocs.org/sdr/DALA2018032601904.md): Battery Pack · inoperative · Mar 25, 2018 · N906AT · Boeing 717200 · Emergency Lighting
  > EMERGENCY CEILING LIGHTS ARE INOPERATIVE BETWEEN SEAT ROWS 1 AND 13. MAINTENANCE REPLACED THE BATTERY PACK IAW AMM 33-51-03. EMERGENCY LIGHT OPS NORMAL.
- [SDR DALA2016082506196](https://openairdocs.org/sdr/DALA2016082506196.md): Door Frame · cracked · Aug 24, 2016 · N906AT · Boeing 717200 · Passenger/Crew Doors
  > RIGHT FORWARD GALLEY SERVICE DOOR, LOWER FORWARD CORNER, LOWER HORIZONTAL FRAME CRACKED. REPLACED GALLEY SERVICE DOOR LOWER HORIZONTAL FRAME IAW SRM 51-41-02, 51-41-05, B DWG 5910084, REINSTALLED R1 DOOR IAW AMM 52-42-01 000-801, 52-42-01 400-801, PRESSURE CH
- [SDR DALA2017010500109](https://openairdocs.org/sdr/DALA2017010500109.md): Seal Depressor · damaged · Aug 23, 2016 · N906AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > FOUND AFT LOWER SEAL DEPRESSOR TO BE DAMAGED. COMPLIED WITH PRI 549608-14, AND ER/A 549608-14. BY FABRICATING PROTECTING & INSTALLATION OF AFT SEAL DEPRESSOR ON AFT CARGO DOOR CUTOUT.
- [SDR DALA2016110208149](https://openairdocs.org/sdr/DALA2016110208149.md): Skin · corroded · Aug 23, 2016 · N906AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > SKIN CORRODED AFT OF BS 1002 ABOVE STRINGER 26. BLENDED AREA IAW SRM 53-00-00 FIG 103. FOUND TO BE OUT OF LIMITS. REPAIRED IAW ER/A 54713-14 REV O.
- [SDR DALA2016082406194](https://openairdocs.org/sdr/DALA2016082406194.md): Door Frame · cracked · Aug 23, 2016 · N906AT · Boeing 717200 · Fuselage Main, Structure
  > AFT CARGO INTERNAL FUSELAGE CUT OUT, LOWER DOOR JAMB PAN HAS NUMEROUS AREAS OF CORROSION THAT IS AROUND THE AFT CAM LATCH FITTING AND LOWER AFT STOP ASSY TO THE FWD LOWER AFT STOP AND FWD CAM LATCH FITTINGS INCLUDING SPLICES. AROUND BARREL NUTS, AND THE 2 LOW
- [SDR DALA2016082306153](https://openairdocs.org/sdr/DALA2016082306153.md): Skin · cracked · Aug 22, 2016 · N906AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN CRACKED BS 1076 STRINGER 14R. REPAIRED THE SKIN IAW ER/A 547505-14.
- [SDR DALA2016082306152](https://openairdocs.org/sdr/DALA2016082306152.md): Intercostal · corroded · Aug 22, 2016 · N906AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > FOUND INTERCOSTAL ABOVE LONGERON 28R, BS 1002-1022 TO BE CORRODED. REPLACED THE INTERCOSTAL IAW SRM 51-41-02 ORIGINAL, FOUND TO BE OUT OF LIMITS IAW SRM 53-00-00 FIG 103.
- [SDR DALA2016082306154](https://openairdocs.org/sdr/DALA2016082306154.md): Support Angle · cracked · Aug 20, 2016 · N906AT · Boeing 717200 · Passenger/Crew Doors
  > SUPPORT ANGLE IS CRACKED INSIDE L1 DOOR FWD SIDE AT UPPER STOP. REPLACED SUPPORT ANGLE IAW SRM 51-41-02 PG 40 PARA B, 51-41-02 PG 1 PARA 4, AND 51-41-05 PG 17 PARA 8.

Next page: https://openairdocs.org/aircraft/N906AT/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 = 'N906AT' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N906AT/reports

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