# Service difficulty reports: N816AT, cancelled Jan 29, 2003 A list on [N816AT, cancelled Jan 29, 2003](https://openairdocs.org/deregistered/N816AT-2003-01-29.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR AT0200039](https://openairdocs.org/sdr/AT0200039.md): Wire · cut · Mar 23, 2002 · N816AT · Doug DC932 · Light System Wiring > CONE HANDLE EMERGENCY PATH LIGHT AND FORWARD CATWALK, EMERGENCY PATH LIGHT WIRES WERE CUT OFF. REPAIRED WIRES L9045-20, L9054-20N, L9049-20 AND L9057-20N AT CONE HANDLE EMERGENCY PATH LIGHT AND FORWARD CATWALK EMERGENCY PATH LIGHT IAW WDM 33-51-03 AND MM 20-5 - [SDR AT0100077](https://openairdocs.org/sdr/AT0100077.md): Engine · failed · Feb 8, 2001 · N816AT · Doug DC932 · Engine (Turbine/Turboprop) > ON CLIMBOUT CAPTAIN REPORTED NR 2 ENGINE PARAMETERS ACCELERATED WITH N1/N2 CLIMBING THRU 99 PERCENT AND EGT AT 750C FOR 30 SECONDS. SHUT DOWN ENGINE AND SECURED AIRCRAFT FOR ENGINE OUT APPROACH. REMOVED AND REPLACED NR 2 ENGINE DUE TO EGT LIMITS EXCEEDING TE - [SDR AT0000152](https://openairdocs.org/sdr/AT0000152.md): Light · inoperative · Jun 8, 2000 · N816AT · Doug DC932 · Emergency Lighting > FOUND FLOOR PATH LIGHTS AND NACELLE EMERGENCY LIGHTS OUT. TIGHTENED TERMINAL B2 ON FORWARD ATT SWITCH. REMOVED AND REPLACED RIGHT BATTERY PACK AND CHARGED LEFT BATTERY PACK IAW DC9 MM 33-51-01. - [SDR AT0000264](https://openairdocs.org/sdr/AT0000264.md): Door Frame · cracked · May 7, 2000 · N816AT · Doug DC932 · Fuselage Miscellaneous Structure > DURING A SCHEDULED INSPECTION AT AVBORNE IN MIAMI FL, FOUND FORWARD ENTRANCE DOOR AFT TOP DOOR STOP BOLT HOLES CRACKED. INSTALLED REPAIR DOUBLER IAW RES 00-0408. - [SDR AT0000262](https://openairdocs.org/sdr/AT0000262.md): Keelbeam · cracked · May 2, 2000 · N816AT · Doug DC932 · Fuselage Main, Keel > DURING A SCHEDULED INSPECTION AT AVBORNE IN MIAMI FL., FOUND KEEL BEAM WEB CRACKED AT BS 700 AFT OF GEAR DOOR ACTUATOR. INSTALLED REPAIR IAW RES 00-00441. - [SDR AT0000265](https://openairdocs.org/sdr/AT0000265.md): Skin · damaged · Apr 26, 2000 · N816AT · Doug DC932 · Fuselage Main, Plate/Skin > DURING A SCHEDULED INSPECTION AT AVBORNE IN MIAMI FL., FOUND PREVIOUS REPAIR AT STATION 218 LEFT BELOW LONGERON 15. REPLACED PREVIOUS REPAIR IAW RES 00-0439. - [SDR AT9900132](https://openairdocs.org/sdr/AT9900132.md): Intercostal · misdrilled · Feb 5, 1999 · N816AT · Doug DC932 · Fuselage Miscellaneous Structure > SCHEDULED INSPECTION AT AERO CORP, FL, FOUND THE FORWARD CARGO COMPARTMENT AT STA 370 TO STA 375 L-29R INTERCOASTAL UPPER FLANGE AND WEB HAS MISDRILLED FASTENER HOLES. FABRICATED NEW INTERCOASTAL, FIT, DRILLED, TREATED AND PRIMED. LOCATED NEW WEB, DRILLED, D - [SDR AT9900134](https://openairdocs.org/sdr/AT9900134.md): Support · cracked · Feb 2, 1999 · N816AT · Doug DC932 · Fuselage Miscellaneous Structure > SCHEDULED INSPECTION AT AERO CORP, FL, FOUND FORWARD CARGO COMPARTMENT STA 351 TO STA 370 L-29L INTERCOASTAL BENT, AND FLOOR SUPPORT WAS FOUND CRACKED. REMOVED AND FABRICATED NEW INTERCOASTAL, RECEIVED NEW SUPPORT, DRILLED, AND INSTALLED BOTH PARTS IAW DC9 SR - [SDR AT9900136](https://openairdocs.org/sdr/AT9900136.md): Skin · creased · Feb 1, 1999 · N816AT · Doug DC932 · Fuselage Main, Plate/Skin > SCHEDULED INSPECTION AT AERO CORP, FL. FOUND A CREASE OUT OF LIMITS AT STA 484 RIGHT SIDE L-19-20. ALSO, A COAX CABLE STAND OFF BROKEN AT STA 955 ABOVE L-20R. TRIMMED OUT CREASE, FABRICATED AND INSTALLED DOUBLER IAW DC9 SRM 51-30-5, 51-30-2, 53-04 FIG 12B, - [SDR AT9900082](https://openairdocs.org/sdr/AT9900082.md): Skin · dented · Jan 30, 1999 · N816AT · Doug DC932 · Entrance Stairs > SCHEDULED INSPECTION AT AERO CORP, FL. FOUND NUMEROUS DENTS IN AFT VENTRAL STAIRS LOWER AFT SKIN FROM SPLICE. REMOVED AND REPLACED EXISTING SKIN FROM PREVIOUS SPLICE IAW DC9 SRM 51-10-4, 51-30-2, AND RES NR 99221. - [SDR AT9900129](https://openairdocs.org/sdr/AT9900129.md): Cusp · corroded · Jan 29, 1999 · N816AT · Doug DC932 · Fuselage Miscellaneous Structure > SCHEDULED INSPECTION AT AERO CORP, FL. CORROSION WAS FOUND ON CUSP MEMBRANE AT RIGHT OUTBOARD STA 945 AND STA 965 CUSP A7. REMOVED CORROSION AND FABRICATED DOUBLERS AND FILLER IAW DC9 SRM 51-30-2, 51-10-3, 53-20-1. DOUBLER (P/N 1A-42076-1) OFF. - [SDR AT9900128](https://openairdocs.org/sdr/AT9900128.md): Longeron · corroded · Jan 28, 1999 · N816AT · Doug DC932 · Fuselage Main, Longeron/Stringer > SCHEDULED INSPECTION AT AERO CORP, FL. FOUND CORROSION ON LONGERONS AT STA 237 L-30 AND STA 560 TO STA 579 L-30. ALSO, CORRODED RIVETS AT T-CAP AT STA 598 L-24L TO L-24R. REMOVED AND REPLACED FASTENERS ON T-CAP, TREATED CORROSION, CUT OUT DAMAGE LONGERON SE - [SDR AT9900126](https://openairdocs.org/sdr/AT9900126.md): Doubler · corroded · Jan 28, 1999 · N816AT · Doug DC932 · Fuselage Miscellaneous Structure > SCHEDULED INSPECTION AT AERO CORP, FL. FOUND CORROSION BULGED AT STA 937 L-26R. MECHANICALLY REMOVED CORROSION, FASTENERS AND DOUBLER. FABRICATED AND INSTALLED FASTENERS, DOUBLER IAW DC9 SRM 51-30-5, 51-30-2, 51-20-0, AND RES NR 99301. - [SDR AT9900127](https://openairdocs.org/sdr/AT9900127.md): Structure · corroded · Jan 21, 1999 · N816AT · Doug DC932 · Fuselage Main, Structure > SCHEDULED INSPECTION AT AERO CORP, FL. FOUND CORROSION ON THE FORWARD AND AFT CARGO COMPARTMENT. LOCATIONS ARE AS FOLLOW: CARGO DOOR FRAME LOWER EDGE AT STA 340 TO 427, FRAME STA 522 L-28L TO L-28R, AFT CARGO WEB STA 870 L-29R ON LEFT AND RIGHT SIDE, AFT CA - [SDR AT9900135](https://openairdocs.org/sdr/AT9900135.md): Skin · cracked · Jan 20, 1999 · N816AT · Doug DC932 · Fuselage Main, Plate/Skin > SCHEDULED INSPECTION AT AERO CORP, FL. FOUND A CRACK ON UPPER NOSE SKIN RIGHT SIDE AT STA 69.5 AT SECOND FASTENER JUST TO THE RIGHT OF PREVIOUS REPAIR. REMOVED EXISTING FILLER, FASTENERS, ENLARGED EXISTING CUTOUT TO REMOVED CRACK, FABRICATED, TREATED, PRIMED - [SDR AT9900138](https://openairdocs.org/sdr/AT9900138.md): Structure · corroded · Jan 19, 1999 · N816AT · Doug DC932 · Fuselage Main, Structure > SCHEDULED INSPECTION AT AERO CORP, FL. FOUND VARIOUS LOCATIONS WITH CORROSION, DELAMINATION AND ELONGATED HOLES. FIRST, AT THE FORWARD CARGO SIDE WALL STRAPS (4 EACH) AND THRESHOLD DOOR STRAP (AFT SIDE) CORRODED AND ENLONGATED HOLES. SECOND, AT THE E/E COMP - [SDR AT9900125](https://openairdocs.org/sdr/AT9900125.md): Frame · cracked · Jan 19, 1999 · N816AT · Doug DC932 · Fuselage Main, Frame > SCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE LEFT MAIN FRAME LOWER FORWARD POCKET AND LOWER FLANGE IN THE WHEEL WELL AT STA 718 CRACKED. REMOVED AND REPLACED MAIN FRAME IAW EO 12-5511-29-B1044, EO 12-5511-29-B1044, AND SB 53-131 R4. FRAME (P/N 9919619-50 - [SDR AT9900103](https://openairdocs.org/sdr/AT9900103.md): Frame · cracked · Jan 9, 1999 · N816AT · Doug DC932 · Fuselage Main, Frame > SCHEDULED INSPECTION AT AERO CORP, FL, FOUND A CRACK AT MAIN FRAME STA 718 RUNNING THROUGH 2 EA FASTENERS IN THE FORWARD INMEDIATE POCKET. REMOVED FITTING, DRILLED UP NEW FITTING, DEBURRED, ALODINED, PRIMED AND INSTALLED IAW DC9 SRM 51-30-1, 51-30-2, 51-30-5, - [SDR AT9900133](https://openairdocs.org/sdr/AT9900133.md): Splice · cracked · Jan 1, 1999 · N816AT · Doug DC932 · Wing Miscellaneous Structure > SCHEDULED INSPECTION AT AERO CORP, FL, FOUND LEFT WING STA XOS 290.0 LEADING EDGE SKIN SPLICE CRACKED. REMOVED AND REPLACED SPLICE PLATE, FABRICATED SPLICE PLATE, DRILLED, DEBURRED, TREATED, PRIMED, AND INSTALLED IAW DC9 SRM 51-10-2 AND RES NR 99199. ## 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 = 'N816AT' AND deregistration_id = 'N816AT-2003-01-29' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N816AT-2003-01-29/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.