# Service difficulty reports: N992AT

A list on [N992AT](https://openairdocs.org/aircraft/N992AT.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 · 170 reports

- [SDR DALA2026081104626](https://openairdocs.org/sdr/DALA2026081104626.md): Power Supply · inoperative · Aug 11, 2026 · N992AT · Boeing 717200 · Emergency Lighting
  > FOUND AFT BULKHEAD DOOR EMERGENCY LIGHT INOPERATIVE. R & R AFT CENTER EMERGENCY LIGHT POWER SUPPLY AND BATTERY IAW AMM 33-51. CHECKS GOOD. OK FOR SVC.
- [SDR DALA2026031101693](https://openairdocs.org/sdr/DALA2026031101693.md): Proximity Sensor · faulted · Mar 10, 2026 · N992AT · Boeing 717200 · Landing Gear Position and Warning
  > ATB- GEAR UNSAFE INDICATION WITH GEAR HANDLE UP. CORRECTIVE ACTION: REPLACED BOTH GEAR UP AND LATCHED PROX SENSORS. ADJUSTED LEFT DOOR LATCH. REPLACED LEFT DOOR LOCK TAB. ALL CHECK NORMAL.(8283248)
- [SDR DALA2026030501522](https://openairdocs.org/sdr/DALA2026030501522.md): Switch · faulted · Mar 3, 2026 · N992AT · Boeing 717200 · Landing Gear Position and Warning
  > WORKING IB LOG 8283224 RED LINED IN ERROR. R & R THE PSEU IAW AMM 32-61-01 & LG SWITCH IAW AMM 32-62-03 (8283225)
- [SDR DALA2025121509135](https://openairdocs.org/sdr/DALA2025121509135.md): Cover · unsecure · Dec 11, 2025 · N992AT · Boeing 717200 · Emergency Exits
  > TAIL EMG EXIT NEEDS RESECURING. REPLACED AFT EIXT ARMING COVER PER B717 AMM 52-12 (7940018)
- [SDR DALA2025111208302](https://openairdocs.org/sdr/DALA2025111208302.md): Oil System · leaking · Nov 11, 2025 · N992AT · Boeing 717200 · APU Oil System
  > SMKE - AFTER STARTING APU AND TURNING ON PACKS, CABIN FILLED WITH ACRID, RUBBERY, BURNING VISIBLE SMOKE. TURNED OFF PACKS AND SMOKE DISSIPATED. FOUND APU OIL TANK EMPTY AND BLEED DUCTS CONTAMINATED WITH OIL. CLEANED BLEED DUCTS, REPLACED COALESCER BAGS AND PE
- [SDR DALA2025102207717](https://openairdocs.org/sdr/DALA2025102207717.md): Seal · fod · Oct 20, 2025 · N992AT · Boeing 717200 · Service Doors
  > DIVERTED TO BOS DUE TO R1 GALLEY DOOR HIGH PITCH SQUEAL. CLEANED DEBRIS & LUBED DOOR SEAL, PRESSURIZED AIRCRAFT. NO DEFECTS NOTED.(7584826)
- [SDR DALA2025062604792](https://openairdocs.org/sdr/DALA2025062604792.md): Coalescer Bag · contaminated · Jun 25, 2025 · N992AT · Boeing 717200 · Humidity Control System
  > SHIP 9535 STARTED APU AND DIRTY, MUSTY SMELL OCCURRED ONCE AIR CAME ON. CALLED MX, UNABLE TO FIX IMEDIATLY. CORRECTIVE ACTION: COALESCER BAGS SOAK IN WATER AND DIRTY CAUSE THE ODOR IN CABIN. FOUND DRAIN LINE CLOGGED AND UNCLOGGED LINE. RAN APU FOR 2 HOURS WITH
- [SDR DALA2024122311964](https://openairdocs.org/sdr/DALA2024122311964.md): Skin · damaged · Dec 20, 2024 · N992AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > FUSELAGE DAMAGE AFT OF L1 DOOR. REPAIRED A/C PER ER/A 542469-14 REV A. REF 001-0002:0514-2000 NRC 6 FOR DOCUMENTATION OF WORK PERFORMED. (LP #6956730)
- [SDR DALA2024122311962](https://openairdocs.org/sdr/DALA2024122311962.md): Skin · ground damage · Dec 20, 2024 · N992AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > AIRCRAFT SUSTAINED DAMAGE FROM JETWAY CONTACT AT LH FRAME STATION BS 237 BETWEEN STR 18L AND STR 17LH. SUMMARY NRC 001-0002:0514-2001/006 00006: COMPLIED WITH ER/A 542469-14 REV A. ENSURED PRI 542469-14 REV 0 MATCHES FINAL ERA. (LP #0719406)
- [SDR DALA2024122311965](https://openairdocs.org/sdr/DALA2024122311965.md): None · none · Dec 19, 2024 · N992AT · Boeing 717200 · Standard Practices/Structures
  > DTE TRACKING PER ER/A 542469-14 REV A. REPAIR APPROVAL IS LIMITED TO 12 MONTHS OF SERVICE. ER/A REVISION REQUIRED FOR SERVICE BEYOND THIS LIMIT. DTA REQUIRED IN ACCORDANCE WITH FAA AC 120-93. REPAIR APPROVAL LIMITED TO 12 MONTHS OF SERVICE AFTER ACCOMPLISHMENT
- [SDR DALA2024022302565](https://openairdocs.org/sdr/DALA2024022302565.md): Fairing · missing · Jan 9, 2024 · N992AT · Boeing 717200 · Nacelle/Pylon, Main Frame
  > THE #2 ENGINE WAS EXPERIENCING HIGH OIL CONSUMPTION. DURING THE INVESTIGATION, WHEN THE #2 ENGINE COWLS WERE OPENED, MAINTENANCE DISCOVERED THAT THE LOWER LEFT COMPRESSOR FAIRING WAS MISSING. EVIDENCE SHOWS THAT THE FAIRING ATTACHING INSERTS LOOKED TO BE "PULL
- [SDR DALA2024010800321](https://openairdocs.org/sdr/DALA2024010800321.md): Unknown · unknown · Jan 5, 2024 · N992AT · Boeing 717200 · Emergency Lighting
  > THE EXTERIOR EMERGENCY ILLUMINATION SYSTEM IS INOPERATIVE. MAINTENANCE FOUND DAMAGE ON PCB OF POWER SUPPLY. THE PCB OF POWER SUPPLY WAS REPLACED PER B717 AMM 33-51. ALSO REPLACED THE EMERGENCY BATTERY AS A PRECAUTION PER B717 AMM 33-51. ALL LIGHT OPERATIONALLY
- [SDR DALA2023071205665](https://openairdocs.org/sdr/DALA2023071205665.md): Unknown · unknown · Jul 12, 2023 · N992AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > CORROSION TYPE EXFOLATION ON FUSELAGE SKIN (LOWER CUTOUT) AT AFT CARGO COMPARTMENT STA 974. SUMMARY OF NRC 00512: CORROSION LEVEL 2. FUSELAGE SKIN LOWER CUTOUT AT AFT CARGO COMPARTMENT STA 974 WAS REPAIRED PER PRI 610235-14 REV 1 AND ER/A 610235-14 REV ORIGINA
- [SDR DALA2023080406299](https://openairdocs.org/sdr/DALA2023080406299.md): Unknown · unknown · Jul 11, 2023 · N992AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > ER/A 610235-14; FUSELAGE SKIN AFT CARGO DOOR CUTOUT SKIN AND DOUBLER STA Y=954 TO 994, L-28R IS CORRODED. SUBJECT REPAIR REQUIRES FOLLOW-ON ACTION. ACCOMPLISH ER/A 610235-14, SECTION II REPETITIVE INSPECTION WITHIN 8,000 FLIGHT CYCLES FROM 32,098 TOTAL FLIGHT
- [SDR DALA2023071205663](https://openairdocs.org/sdr/DALA2023071205663.md): Unknown · unknown · Jul 9, 2023 · N992AT · Boeing 717200 · Fuselage Main, Frame
  > CORROSION ON FRAME STA Y=1021 LONGERON 30+1.5 IN RH/LH. SUMMARY OF NRC 00513: CORROSION LEVEL 2. FRAME STA Y=1021 LONGERON 30 WAS REPAIRED PER B717 SRM 53-20-07-2R PROCEDURE 3, REPAIR 3. (LP #2857160)
- [SDR DALA2023071205661](https://openairdocs.org/sdr/DALA2023071205661.md): Unknown · unknown · Jul 8, 2023 · N992AT · Boeing 717200 · Fuselage Structure (General)
  > CORROSION ON RH ANGLE CUSP FROM STA Y=200 TO Y=219 AT PAX CABIN. SUMMARY OF NRC 00253: CORROSION LEVEL 2. RH ANGLE CUSP FROM STA Y=160 TO Y=219 WAS REPAIRED PER ERA 609394-14 REV ORIGINAL SECTION I. PERMANENT REPAIR. ASSOCIATED ER/A 14-609394 ADDED FOR AC 9535
- [SDR DALA2023070405374](https://openairdocs.org/sdr/DALA2023070405374.md): Unknown · unknown · Jul 3, 2023 · N992AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION ON INTERCOSTAL BTW STA Y=946-954 AND LONGERON 30 TO 29RH AT AFT CARGO COMPARTMENT (C2). SUMMARY OF NRC 00181: CORROSION LEVEL 2. INTERCOSTAL BTW STA Y=946-954 AND LONGERON 30 TO 29RH AT AFT CARGO COMPARTMENT (C2) WAS REPLACED PER B717 SRM 51-41-02-0G
- [SDR DALA2023070405373](https://openairdocs.org/sdr/DALA2023070405373.md): Unknown · unknown · Jul 3, 2023 · N992AT · Boeing 717200 · Fuselage Structure (General)
  > CORROSION ON DOOR JAMB SEVERAL POINTS AT AFT COMPARTMENT (C2). SUMMARY OF NRC 00176: CORROSION LEVEL 2. DOOR JAMB AT AFT COMPARTMENT WAS REPLACED PER B717 SRM 51-41-02-0G & 51-41-05-0G. (LP #2848116)
- [SDR DALA2023070405370](https://openairdocs.org/sdr/DALA2023070405370.md): Unknown · unknown · Jul 3, 2023 · N992AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CRACK ON INTERCOSTAL STA 636 X=0 CEILING AREA, FWD CARGO. SUMMARY OF NRC 00507: INTERCOSTAL STA 636 X=0 CEILING AREA WAS REPAIRED PER B717 SRM 51-70-11-2R PROCEDURE 1. (LP #2847519)
- [SDR DALA2023070305309](https://openairdocs.org/sdr/DALA2023070305309.md): Unknown · unknown · Jul 3, 2023 · N992AT · Boeing 717200 · Fuselage Main, Frame
  > CORROSION ON WEB SEVERAL POINTS AT AREA DOOR AFT COMPARTMENT (ENTRY AREA) (C2). SUMMARY OF NRC 00175: CORROSION LEVEL 2. WEB AREA DOOR AFT COMPARTMENT WAS REPLACED PER B717 SRM 51-41-02-0G & 51-41-05-0G. (LP #2846580)
- [SDR DALA2023070305308](https://openairdocs.org/sdr/DALA2023070305308.md): Unknown · unknown · Jul 3, 2023 · N992AT · Boeing 717200 · Fuselage Main, Longeron/Stringer
  > CORROSION ON FRAME CLIP STA 1002 LONGERON 29RH TO 29LH AT AFT CARGO. SUMMARY OF NRC 00496: CORROSION LEVEL 2. FRAME CLIP STA 1002 LONGERON 29RH TO 29LH WAS REPLACED PER B717 SRM 51-41-02-0G. (LP #2846532)
- [SDR DALA2023070305305](https://openairdocs.org/sdr/DALA2023070305305.md): Unknown · unknown · Jul 1, 2023 · N992AT · Boeing 717200 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK ON STA 545 TO STA 560 WAS FOUND CORRODED OUT OF LIMITS PER B717 SRM 53-20-52-1A PROCEDURE 1. SUMMARY OF NRC 00473: CORROSION LEVEL 2. SEAT TRACK ON STA 532 TO 588 WAS REPAIRED PER B717 SRM 53-20-52-2R PROCEDURE 5 REPAIR 5. (LP #2844557)
- [SDR DALA2023070305301](https://openairdocs.org/sdr/DALA2023070305301.md): Unknown · unknown · Jul 1, 2023 · N992AT · Boeing 717200 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON RH INBD SEAT TRACK STA Y=215 TO Y=220 AT PAX CABIN. SUMMARY OF NRC 00251: CORROSION LEVEL 2. RH INBD SEAT TRACK STA Y=215 TO Y=220 WAS REPAIRED PER B717 SRM 53-20-52-2R PROCEDURE 5 REPAIR 5. (LP #2843578)
- [SDR DALA2023070305300](https://openairdocs.org/sdr/DALA2023070305300.md): Unknown · unknown · Jun 30, 2023 · N992AT · Boeing 717200 · Fuselage Floor Panel
  > CORROSION ON FLOOR SUPPORT STA Y=175 BTW X=-20 AND X=-45 AT PAX CABIN W1. SUMMARY OF NRC 00309: CORROSION LEVEL 2. FLOOR SUPPORT STA Y=175 BTW X=-20 AND X=-45 AT PAX CABIN WAS REPLACED PER B717 SRM 51-41-05-0G PAR 8 & 51-41-02-0G PAR 4. (LP #2843312)
- [SDR DALA2023070305298](https://openairdocs.org/sdr/DALA2023070305298.md): Unknown · unknown · Jun 30, 2023 · N992AT · Boeing 717200 · Fuselage Main, Frame
  > CORROSION ON FITTING STA 893.5 BELOW FLOOR LEVEL CUSP WEB AREA WAS FOUND. SUMMARY OF NRC 00503: CORROSION LEVEL 2. FITTING SPLICE ON STA 893.5 RH WAS REPLACED PER DWG 9910151 REV CH AND B717 SRM 51-41-05-0G. (LP #2842912)
- [SDR DALA2023062905211](https://openairdocs.org/sdr/DALA2023062905211.md): Unknown · unknown · Jun 28, 2023 · N992AT · Boeing 717200 · Fuselage Main, Frame
  > AFTER CORROSION REMOVAL ON CUSP WEB (LIGHTNING HOLE) STA 539, STA 648, STA 890 TO 907, AND STA 929 TO 935 AREAS WERE FOUD OUT OF LIMITS PER B717 SRM 53-00-55-1A PROCEDURE 1 ALLOWABLE DAMAGE 1 PAR 4 A. SUMMARY OF NRC 00480: CORROSION LEVEL 2. (LIGHTNING HOLE) S
- [SDR DALA2023062805189](https://openairdocs.org/sdr/DALA2023062805189.md): Unknown · unknown · Jun 28, 2023 · N992AT · Boeing 717200 · Fuselage Main, Frame
  > EXFOLIATION CORROSION ON DIAPHRAGM STA Y=178 TO Y=198 X=-45 X=-52 AT PAX CABIN W1. SUMMARY OF NRC 00303: CORROSION LEVEL 2. DIAPHRAGM STA Y=178 TO Y=198 X=-45 TO X=-52 WAS REPLACED PER B717 SRM 51-41-02-0G. (LP #2838515)
- [SDR DALA2023070305297](https://openairdocs.org/sdr/DALA2023070305297.md): Unknown · unknown · Jun 27, 2023 · N992AT · Boeing 717200 · Fuselage Floor Panel
  > BROKEN FLOOR PANEL 121MF OF FWD CARGO COMPARTMENT (C1). SUMMARY OF NRC 00470: FLOOR PANEL 121MF WAS MANUFACTURED AND REPLACED PER ERA 544901-14 REV A AND INSTALLATION OF FLOOR PANEL 121MF ACCOMPLISHED UNDER TASK CARD 2040-0006. (LP #2837740)
- [SDR DALA2023062805188](https://openairdocs.org/sdr/DALA2023062805188.md): Unknown · unknown · Jun 27, 2023 · N992AT · Boeing 717200 · Fuselage Main, Frame
  > CRACKS ON CUSP WEB STA Y=715 AND Y=897 BELOW SEAT TRACK LBL=44 AT PASSENGER CABIN (CPAX). SUMMARY OF NRC 00265: CUSP WEB STA Y=715 AND Y=897 LBL=44 AT PASSENGER CABIN WERE REPAIRED PER B717 SRM 53-00-55-2R-4 PAR. 5 FIG 221 AND FIG 226. (LP #2837755)
- [SDR DALA2023062805186](https://openairdocs.org/sdr/DALA2023062805186.md): Unknown · unknown · Jun 27, 2023 · N992AT · Boeing 717200 · Fuselage Main, Longeron/Stringer
  > CORROSION ON WIRING CLIPS STA Y=272, Y=291, Y=305, Y=310, Y=539, Y=648, Y=849, Y=875, & Y=885 LBL=57 ALSO Y= 885, Y=886, Y=835, Y=845, Y=848, Y=648, Y=575, Y=737, Y=346, & Y= 309 RBL=57 AT PASSENGER CABIN (CPAX). SUMMARY OF NRC 00266: CORROSION LEVEL 2. WIRING
- [SDR DALA2023062805182](https://openairdocs.org/sdr/DALA2023062805182.md): Unknown · unknown · Jun 26, 2023 · N992AT · Boeing 717200 · Fuselage Floor Panel
  > CRACKS ON PAN FWD INNER SIDE PROJECTION BEAMS 1, 3, & 5 AT FWD CARGO COMPARTMENT. SUMMARY OF NRC 00372: PAN FWD INNER SIDE PROJECTION BEAMS 1, 3, & 5 AT FWD CARGO COMPARTMENT WERE REPAIRED PER B717-200 SRM 52- 30-02-2R PROCEDURE 1 REPAIR 1. (LP #2836257)
- [SDR DALA2023062805181](https://openairdocs.org/sdr/DALA2023062805181.md): Unknown · unknown · Jun 26, 2023 · N992AT · Boeing 717200 · Fuselage Main, Frame
  > CORROSION ON ANGLE AT L1 DOOR JAM WEB (AFT) STA Y=200 AT PAX CABIN. SUMMARY OF NRC 00438: CORROSION LEVEL 2. ANGLE AT L1 DOOR JAM WEB AFT STA Y=200 AT PAX CABIN WAS REPLACED PER B717 SRM 51-41-05-0G AND 51-41-02-0G. (LP #2835840)
- [SDR DALA2023070305296](https://openairdocs.org/sdr/DALA2023070305296.md): Unknown · unknown · Jun 25, 2023 · N992AT · Boeing 717200 · Fuselage Main, Frame
  > CORROSION WAS FOUND ON ANGLE BTW STA Y=149 TO Y=160 AND RBL 56 AT R1 DOOR CUTOUT AREA. (CPAX). SUMMARY OF NRC 00460: CORROSION LEVEL 2. ANGLE BTW STA Y=149 TO Y=160 AND RBL 56 WAS REPLACE PER DWG 5910085 REV. DJ. ANGLE BTW STA Y=149 TO Y=160 AND RBL 56 AT R1 D
- [SDR DALA2023062805179](https://openairdocs.org/sdr/DALA2023062805179.md): Unknown · unknown · Jun 25, 2023 · N992AT · Boeing 717200 · Fuselage Main, Frame
  > AFTER CORROSION REMOVAL AT THE EDGES OF LIGHTENING HOLE ON CUSP; WEBS AT STA Y=469, Y=508, Y=518, Y=527, Y=546, AND X=58 WERE FOUND OUT LIMITS PER B717 SRM 53-00-00-1A PROCEDURE ALLOWABLE DAMAGE GENERAL PAR. 4.A. SUMMARY OF NRC 00478: CORROSION LEVEL 2. CUSP W
- [SDR DALA2023062805178](https://openairdocs.org/sdr/DALA2023062805178.md): Unknown · unknown · Jun 25, 2023 · N992AT · Boeing 717200 · Fuselage Main, Frame
  > AFTER CORROSION REMOVAL, THE EDGES OF LIGHTENING HOLES ON CUSP WEBS AT STA Y=461, Y=488, Y=585, Y=799, TO Y=809; LBL X=58 WERE FOUND OUT LIMITS PER B717 SRM 53-00-00-1A PROCEDURE ALLOWABLE DAMAGE GENERAL PAR. 4.A. SUMMARY OF NRC 00481: CORROSION LEVEL2. CUSP W
- [SDR DALA2023062805176](https://openairdocs.org/sdr/DALA2023062805176.md): Unknown · unknown · Jun 24, 2023 · N992AT · Boeing 717200 · Fuselage Main, Longeron/Stringer
  > AFTER CORROSION REMOVAL AT LONGERON 30, STA 965.5 TO 967.5 AND STA 972.5 TO 973.5 WAS FOUND OUT OF LIMITS PER B717 SRM 53-00-00-1A PROCEDURE ALLOWABLE DAMAGE GENERAL PAR. 4.C.(2). SUMMARY OF NRC 00449: CORROSION LEVEL 2. LONGERON 30 BTW STA 965.5 TO 973.5 WAS
- [SDR DALA2023062805175](https://openairdocs.org/sdr/DALA2023062805175.md): Unknown · unknown · Jun 24, 2023 · N992AT · Boeing 717200 · Fuselage Main, Frame
  > CORROSION REMOVAL ON CUSP WEB STA Y=843 TO Y=846 IS OUT OF LIMITS PER B717 53-00-55-1A PROCEDURE 1 PAR. 4. SUMMARY OF NRC 00492: CORROSION LEVEL 2. CUSP WEB STA Y=843 TO Y=846 WAS REPAIRED PER B717 SRM 53-00-55-2R-4 FIG 215. (LP #2831675)
- [SDR DALA2023062705157](https://openairdocs.org/sdr/DALA2023062705157.md): Unknown · unknown · Jun 23, 2023 · N992AT · Boeing 717200 · Fuselage Floor Panel
  > AFTER CORROSION REMOVAL ON GALLEY FITTING BTW STA Y=200 AND Y=218 BTW X=-20 WAS FOUND OUT OF LIMITS PER B717 SRM 53-00-00-1A ALLOWABLE DAMAGE FIG. 101 (SHEET 2). SUMMARY OF NRC 0053: CORROSION LEVEL 2. SUPPORT WAS REPLACED PER B717-200 SRM 51-41-02-0G AND 51-4
- [SDR DALA2023062705155](https://openairdocs.org/sdr/DALA2023062705155.md): Unknown · unknown · Jun 23, 2023 · N992AT · Boeing 717200 · Fuselage Floor Panel
  > RELATED NRC 261 AFTER CORROSION REMOVAL ON FLOOR SUPPORT STA Y=200 BTW X=6 AND X=-6 FLOOR SUPPORT WAS FOUND OUT OF LIMITS PER B717 SRM 53-00-00-1A ALLOWABLE DAMAGE FIG. 101. SUMMARY OF NRC 00448: CORROSION LEVEL 2. FLOOR SUPPORT STA Y=200 BTW X=6 AND X=-6 WAS
- [SDR DALA2023062305083](https://openairdocs.org/sdr/DALA2023062305083.md): Unknown · unknown · Jun 23, 2023 · N992AT · Boeing 717200 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT TRACK RBL 22 BTW STA 411-413 AT PAX COMPARTMENT. (CPAX). SUMMARY OF NRC 00467: CORROSION LEVEL2. SEAT TRACK RBL 22 BTW STA 411-413 WAS REPAIRED PER B717 SRM 53-20-52-2R PROCEDURE 1 REPAIR 1. (LP #2830244)
- [SDR DALA2023062105025](https://openairdocs.org/sdr/DALA2023062105025.md): Unknown · unknown · Jun 20, 2023 · N992AT · Boeing 717200 · Fuselage Floor Panel
  > EXFOLIATION CORROSION ON FLOOR SUPPORT RH STA Y=198 X=55 LH SIDE AT PAX CABIN. SUMMARY OF NRC 00271: CORROSION LEVEL 2. FLOOR SUPPORT RH STA Y=198 X=55 WAS REPLACED PER B717-200 SRM 51-41-05-0G. (LP #2826207)
- [SDR DALA2023061904973](https://openairdocs.org/sdr/DALA2023061904973.md): Unknown · unknown · Jun 19, 2023 · N992AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION WAS FOUND AT JAM WEB STA Y=200 ON STRINGER 18. SUMMARY OF NRC 00458: CORROSION LEVEL 2. JAM WEB STA Y=200 ON STRINGER 18 WAS REPAIRED PER B717 SRM 51-70-10-2R PROCEDURE 2 REPAIR 2. (LP #2823464)
- [SDR DALA2023061904969](https://openairdocs.org/sdr/DALA2023061904969.md): Unknown · unknown · Jun 17, 2023 · N992AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION ON FLOOR SUPPORT STA Y=200 X=10 AT PAX CABIN W1. SUMMARY OF NRC 00275: CORROSION LEVEL 2. FLOOR SUPPORT STA Y=200 X=10 WAS REPLACED PER B717 SRM 51-41-05-0G. (LP #2821504)
- [SDR DALA2023061904968](https://openairdocs.org/sdr/DALA2023061904968.md): Unknown · unknown · Jun 17, 2023 · N992AT · Boeing 717200 · Fuselage Structure (General)
  > CORROSION ON DIAPHRAGM STA Y=198 TO Y=200 BTW X=-30 AND X=-50 (RH SIDE) AT PAX CABIN. SUMMARY OF NRC 00254: CORROSION LEVEL 2. DIAPHRAGM STA Y=198 TO Y=218 BTW X=-30 AND X=-56 (RH SIDE) WAS REPLACED PER DWG 9936534 REV BW. (LP #2821288)
- [SDR DALA2023061904965](https://openairdocs.org/sdr/DALA2023061904965.md): Unknown · unknown · Jun 16, 2023 · N992AT · Boeing 717200 · Fuselage Structure (General)
  > CORROSION ON DIAPHRAGM FROM STA Y=190 TO Y=200 BTW X=50 AND X=57 (L1 DOOR) AT PAX CABIN. SUMMARY OF NRC 00274: CORROSION LEVEL 2. DIAPHRAGM FROM STA Y=190 TO Y=200 BTW X=50 AND X=57 WAS REPAIRED PER B717 SRM 51-70-10-2R REPAIR 2. (LP #2819862)
- [SDR DALA2023061904964](https://openairdocs.org/sdr/DALA2023061904964.md): Unknown · unknown · Jun 16, 2023 · N992AT · Boeing 717200 · Fuselage Floor Panel
  > CORROSION ON FLOOR SUPPORT STA Y=175 TO Y=198 X=- 45 AT PAX CABIN W1. SUMMARY OF NRC 00290: CORROSION LEVEL 2. FLOOR SUPPORT STA Y=175 TO Y=198 X=-45 AT PAX CABIN WAS REPLACED PER B717 SRM 51-41-02-0G. (LP #2819821)
- [SDR DALA2023061604905](https://openairdocs.org/sdr/DALA2023061604905.md): Unknown · unknown · Jun 16, 2023 · N992AT · Boeing 717200 · Fuselage Structure (General)
  > CRACK ON ANGLE UPPER BEAM AFTER CORNER AT CABIN PAX L1 DOOR. SUMMARY OF NRC 00128: ANGLE UPPER BEAM AFTER CORNER AT CABIN PAX L1 DOOR WAS REPAIRED PER B717-200 SRM 52-10-02-2R PROCEDURE 7, REPAIR 7. (LP #2819045)
- [SDR DALA2023061604902](https://openairdocs.org/sdr/DALA2023061604902.md): Unknown · unknown · Jun 16, 2023 · N992AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION ON FLOOR SUPPORT L1 ENTRANCE DOOR STA Y=180 AND Y=195 AT PAX CABIN W1. SUMMARY OF NRC 00268: CORROSION LEVEL 2. FLOOR SUPPORT L1 ENTRANCE DOOR STA Y=180 AND Y=195 WAS REPLACED PER B717 SRM 51-41-02-0G AND 51-41-05-0G. (LP #2818795)
- [SDR DALA2023061504880](https://openairdocs.org/sdr/DALA2023061504880.md): Unknown · unknown · Jun 15, 2023 · N992AT · Boeing 717200 · Fuselage Main, Frame
  > CRACK CUSP WEB STA Y=218 RBL=54 AT PASSENGER CABIN (CPAX). SUMMARY OF NRC 00272: CUSP WEB STA Y=218 RBL=54 WAS REPAIRED PER B717 SRM 53-00-55-2R REPAIR 4. (LP #2816960)
- [SDR DALA2023061504877](https://openairdocs.org/sdr/DALA2023061504877.md): Unknown · unknown · Jun 14, 2023 · N992AT · Boeing 717200 · Fuselage Main, Frame
  > CRACK ON AFT CARGO DOOR FRAME BTW ANGLE AND LACH AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00092: AFT CARGO DOOR FRAME BTW ANGLE AND LACH AT AFT CARGO COMPARTMENT WAS REPAIRED PER B717-200 SRM 52-30-02-2R PROCEDURE 8 REPAIR 8 FIG 204. (LP #2816372)

Next page: https://openairdocs.org/aircraft/N992AT/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 = 'N992AT' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N992AT/reports

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