# Service difficulty reports: N889AA, cancelled Jan 8, 2003 A list on [N889AA, cancelled Jan 8, 2003](https://openairdocs.org/deregistered/N889AA-2003-01-08.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 · 70 reports - [SDR AALA20012028](https://openairdocs.org/sdr/AALA20012028.md): Light · inoperative · Nov 8, 2001 · N889AA · Boeing 727223 · Emergency Lighting > DFW - DURING OVERNIGHT MAINTENANCE FORWARD SECTION OF EMERGENCY EXIT ESCAPE PATH LIGHTS INOPERATIVE. REPLACED EMERGENCY EXIT ESCAPE PATH LIGHT STRIP IN FORWARD SECTION. SYSTEM GROUND CHECK NORMAL OPERATION. (M) - [SDR AALA20011362](https://openairdocs.org/sdr/AALA20011362.md): Valve · leaking · Jul 3, 2001 · N889AA · Boeing 727223 · Hydraulic Power System > DFW - FLT 1216 - EN ROUTE DFW-PHL, IN FLIGHT B QUANTITY HYDRAULIC SYSTEM AND PRESSURE DECREASED TO ZERO. RETURNED DFW AND LANDED WITHOUT FURTHER INCIDENT. REPLACED RIGHT SIDE ELEVATOR TRANSFER VALVE AND RIGHT SIDE ELEVATOR POWER CONTROL. (M) - [SDR AALA20011354](https://openairdocs.org/sdr/AALA20011354.md): Stiffener · cracked · Jul 2, 2001 · N889AA · Boeing 727223 · Standard Practices/Structures > TUL - FOUND CRACK IN VERTICAL STIFFENER 4 INCHES FROM BOTTOM RIGHT WHEEL WELL AT APU DISCHARGE CUT OUT. REMOVED AND REPLACED VERTICAL STIFFENER PER DRAWING 65-18636 AND ESO 11697 6/28/2001. (M) - [SDR AALA20011353](https://openairdocs.org/sdr/AALA20011353.md): Web · cracked · Jul 2, 2001 · N889AA · Boeing 727223 · Fuselage Structure (General) > TUL - FOUND CRACKS IN STATION 870 WEB EXTENDING FROM FASTENER BELOW LOAD CONTROL VALVE ON BULKHEAD. INSTALLED REPAIR DOUBLER PER SRM 53-10-02. (M) - [SDR AALA20011351](https://openairdocs.org/sdr/AALA20011351.md): Skin · corroded · Jul 2, 2001 · N889AA · Boeing 727223 · Wing, Plate/Skin > TUL - FOUND CORROSION ON LOWER WING SKIN LBL 25 AT STRINGER 6. REMOVED CORROSION. INSTALLED DOUBLER AND TRIPLER PER SRM 57-30-3. (M) - [SDR AALA20011350](https://openairdocs.org/sdr/AALA20011350.md): Skin · corroded · Jun 29, 2001 · N889AA · Boeing 727223 · Wing, Plate/Skin > TUL - FOUND CORROSION ON LOWER WING SKIN AT RBL 18 STRINGER 4. INSTALLED DOUBLER, TRIPLER AND QUAD TRIPLER PER SRM 57-30-3. (M) - [SDR AALA20011366](https://openairdocs.org/sdr/AALA20011366.md): Skin · cracked · Jun 28, 2001 · N889AA · Boeing 727223 · Fuselage Structure (General) > TUL - FOUND FUSELAGE SKIN CRACKED, EXTENDING FROM WIRE BUNDLE ACCESS HOLE DOWN THROUGH AFT LOWER BOLT HOLE. STOP DRILLED CRACK, NDT CHECKED, AND INSTALLED A TITANIUM DOUBLER PER SRM 53-30-3. (M) - [SDR AALA20011352](https://openairdocs.org/sdr/AALA20011352.md): Light · inoperative · Jun 28, 2001 · N889AA · Boeing 727223 · Emergency Lighting > TUL - FOUND AFT VENTRAL STAIR ENTRANCE EMERGENCY EXIT LIGHT DIM DURING 10 MINUTE TEST. REMOVED AND REPLACED EMERGENCY EXIT LIGHT ASSEMBLY. (M) - [SDR AALA20010967](https://openairdocs.org/sdr/AALA20010967.md): Splice · inoperative · May 8, 2001 · N889AA · Boeing 727223 · Emergency Lighting > DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT DIM. REPAIRED EMERGENCY EXIT LIGHT SPLICE. SYSTEM GRUOND CHECKED NORMAL OPERATION. (M) - [SDR AALA20010755](https://openairdocs.org/sdr/AALA20010755.md): Wire · inoperative · Apr 9, 2001 · N889AA · Boeing 727223 · Light System Wiring > DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT ROW 6 DIM. REPLACED EMERGENCY EXIT FLOOR PROXIMITY JUMPER WIRE AT ROW 6. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) - [SDR AALA20010786](https://openairdocs.org/sdr/AALA20010786.md): Light · inoperative · Mar 25, 2001 · N889AA · Boeing 727223 · Emergency Lighting > MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT FORWARD GALLEY INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT STRIP AT FORWARD GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) - [SDR AALA20010040](https://openairdocs.org/sdr/AALA20010040.md): Light · inoperative · Jan 10, 2001 · N889AA · Boeing 727223 · Emergency Lighting > DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT AFT STAIRWAY INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY AT AFT STAIRWAY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) - [SDR AALA20001867](https://openairdocs.org/sdr/AALA20001867.md): Light · damaged · Nov 13, 2000 · N889AA · Boeing 727223 · Emergency Lighting > DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT BETWEEN FIRST CLASS AND COACH CLASS SHORTED. REPAIRED EMERGENCY EXIT LIGHT STRIP BETWEEN FIRST CLASS AND COACH CLASS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) - [SDR AALA20001771](https://openairdocs.org/sdr/AALA20001771.md): Light · inoperative · Oct 30, 2000 · N889AA · Boeing 727223 · Emergency Lighting > DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT AFT STAIRWELL INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY AT AFT STAIRWELL. SYTEM GROUND NORMAL OPERATION. (M) - [SDR AALA20001180](https://openairdocs.org/sdr/AALA20001180.md): Angle · corroded · Jun 29, 2000 · N889AA · Boeing 727223 · Fuselage Miscellaneous Structure > TUL - CORROSION ON FORWARD END OF LEFT SKATE ANGLE, STA 294. SPLICED IN NEW SECTION OF SKATE ANGLE PER SRM 51-20-4 AND ESO 11697 DATED 6-28-00 AND ESO 11697 DATED 6-9-00. (X) - [SDR AALA20001179](https://openairdocs.org/sdr/AALA20001179.md): Stringer · corroded · Jun 28, 2000 · N889AA · Boeing 727223 · Fuselage Main, Longeron/Stringer > TUL - STR 29L KEELBEAM EXTENSION HAS HEAVY CORROSION AT STA 970. INSTALLED.071 INCH 301-1/2 HARD STRAP 3 INCHES BY 21 INCHES WITH HILOCKS PER ESO 11697 DATED 6-27-00. (X) - [SDR AALA991353](https://openairdocs.org/sdr/AALA991353.md): Light · inoperative · Sep 8, 1999 · N889AA · Boeing 727223 · Emergency Lighting > DFW - DURING OVERNIGHT MAINTENANCE, AFT AIRSTAIR EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED AFT AIRSTAIRS EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) - [SDR AALA991317](https://openairdocs.org/sdr/AALA991317.md): Fitting · damaged · Sep 1, 1999 · N889AA · Boeing 727223 · Engine Mount Section > TUL - FOUND 2 UPPER TANG 'F' HOLES ELONGATED AND GOUGED 4 HOLES ELONGATED AT NR 3 ENGINE UPPER FORWARD FITTING. TWO 'E' TAN HOLES OVERSIZED AND FASTENERS INSTALLED 4 'D' HOLES OVERSIZED AND DOUBLER AND TRIPLER INSTALLED PER ESO 11697, DATED 8-27-99 AND 8-31-9 - [SDR AALA991303](https://openairdocs.org/sdr/AALA991303.md): Floorbeam · broken · Aug 27, 1999 · N889AA · Boeing 727223 · Fuselage Main, Floor Beam > TUL - FOUND FLOORBEAM LOWER FLANGE BROKEN COMPLETELY THROUGH THE WIRE BUNDLE STANDOFF SCREW HOLE. INSTALLED ANGLE, EQUAL LEG THICKNESS STAINLESS REPAIR PER SRM 51-40-4 PAGE 5. (M) - [SDR AALA991242](https://openairdocs.org/sdr/AALA991242.md): Light · inoperative · Aug 21, 1999 · N889AA · Boeing 727223 · Emergency Lighting > DFW - DURING OVERNIGHT MAINTENANCE, AFT AIRSTAIRS EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED AFT AIRSTAIRS EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) - [SDR AALA981645](https://openairdocs.org/sdr/AALA981645.md): Stringer · corroded · Sep 8, 1998 · N889AA · Boeing 727223 · Fuselage Main, Longeron/Stringer > TUL - FOUND CORROSION IN STRINGER 28LT STATION 1010-1020, CORROSION OUTBOARD STRINGER 28 LT, STATION 1010-1015. REMOVED DAMAGED STRINGER. INSTALLED STRINGER REPAIR PER SRM 53-10-3 PAGE 4B DETAIL 1, 12 INCHES IN LENGTH. (M) - [SDR AALA981652](https://openairdocs.org/sdr/AALA981652.md): Stringer · corroded · Sep 4, 1998 · N889AA · Boeing 727223 · Fuselage Main, Longeron/Stringer > TUL - FOUND CORROSION IN STRINGER 23R STATION 1148. REMOVED STRINGER 23R FROM 1141-1155 SPLICE IN NEW SECTION AS PER SRM 53-10-3 FIG 1 SHEET 1 PAGE 3. (M) - [SDR AALA981651](https://openairdocs.org/sdr/AALA981651.md): Skin · corroded · Sep 4, 1998 · N889AA · Boeing 727223 · Fuselage Main, Plate/Skin > TUL - FOUND CORROSION ON FUSELAGE SKIN UPPER SURFACE OUTBOARD OF STRINGER 28L STATION 1010-1015 AND BELOW STRINGER 28L, STATION 1010-1015. REMOVED DAMAGED SKIN, INSTALLED REPAIR PER SRM 53-30-3 PAGE 148 FIG 3A. (M) - [SDR AALA981649](https://openairdocs.org/sdr/AALA981649.md): Shear Tie · corroded · Sep 4, 1998 · N889AA · Boeing 727223 · Fuselage Miscellaneous Structure > TUL - FOUND CORROSION ON FORWARD SIDE OF 580 FRAME OUTBOARD OF STRINGER 26L. INSTALLED NEW SHEAR TIE. (M) - [SDR AALA981648](https://openairdocs.org/sdr/AALA981648.md): Floorbeam · corroded · Sep 4, 1998 · N889AA · Boeing 727223 · Fuselage Main, Floor Beam > TUL - FOUND CORROSION 42 INCHES RBL STATION 344, FLOORBEAM LOWER SURFACE. INSTALLED REPAIR AT STATION 344, RBL 12 PER ESO 11697, DATED 8/12/98. (M) - [SDR AALA981647](https://openairdocs.org/sdr/AALA981647.md): Shear Tie · corroded · Sep 4, 1998 · N889AA · Boeing 727223 · Fuselage Miscellaneous Structure > TUL - FOUND CORROSION ON SHEAR TIE STATION 720L BETWEEN 26R AND 27R. INSTALLED NEW SHEAR TIE. (M) - [SDR AALA981644](https://openairdocs.org/sdr/AALA981644.md): Stringer · cracked · Sep 3, 1998 · N889AA · Boeing 727223 · Fuselage Main, Longeron/Stringer > TUL - FOUND STRINGER 15L CRACK JUST FORWARD OF ICE LIGHT HOUSING. REMOVED CRACK AREA OF STRINGER, REPAIRED PER SRM 53-10-3 FIG 5. (M) - [SDR AALA981643](https://openairdocs.org/sdr/AALA981643.md): Stringer · cracked · Sep 3, 1998 · N889AA · Boeing 727223 · Fuselage Main, Longeron/Stringer > TUL - FOUND STRINGER 15L CRACKED JUST AFT OF ICE LIGHT. REMOVED CRACK AREA OF STRINGER AND REPAIRED PER SRM 53-10-3 FIG 5. (M) - [SDR AALA981642](https://openairdocs.org/sdr/AALA981642.md): Floorbeam · corroded · Sep 3, 1998 · N889AA · Boeing 727223 · Fuselage Main, Floor Beam > TUL - FOUND CORROSION 18 INCHES RBL AT STATION 344 BELOW BEAM. REPAIRED TOP OF FLOORBEAM LOWER SIDE BY INSTALLING STRAP PER AAR 53-10-7-2 PAGE 1-3. (M) - [SDR AALA981641](https://openairdocs.org/sdr/AALA981641.md): Floorbeam · corroded · Sep 3, 1998 · N889AA · Boeing 727223 · Fuselage Main, Floor Beam > TUL - FOUND CORROSION ON FLOORBEAM OF FS 380 AND RBL 47 INCHES. INSTALLED REPAIR STRAP PER SRM 53-10-07-2 FIG 1 ON FORWARD SIDE OF FLOORBEAM. (M) - [SDR AALA981640](https://openairdocs.org/sdr/AALA981640.md): Floorbeam · corroded · Sep 3, 1998 · N889AA · Boeing 727223 · Fuselage Main, Floor Beam > TUL - FOUND CORROSION ON TOP CHORD OF FLOORBEAM FS 344 RBL 20 TO LBL 40. REPAIRED DAMAGED AREA OF TOP CHORD FLOORBEAM WITH SPLICE AND REPAIR ANGLES PER SRM 53-10-8 PAGE 49-53. (M) - [SDR AALA981638](https://openairdocs.org/sdr/AALA981638.md): Stiffener · cracked · Sep 3, 1998 · N889AA · Boeing 727223 · Fuselage Miscellaneous Structure > TUL - FOUND CRACK ON RIGHT SIDE OF VERTICLE STIFFENER STATION 1183, RBL 38 WL 239 (INBOARD SIDE OF STIFFENER). INSTALLED REPAIR DOUBLER PER BOEING S/B 727-53-0192 AND DRAWING 65C34406. (M) - [SDR AALA981637](https://openairdocs.org/sdr/AALA981637.md): Stiffener · cracked · Sep 3, 1998 · N889AA · Boeing 727223 · Fuselage Miscellaneous Structure > TUL - FOUND CRACK IN VERTICLE STIFFENER FS 1183, RBL 38 WL 239 OUTBOARD SIDE OF STIFFENER. INSTALLED REPAIR DOUBLER PER BOEING S/B 727-53-0192 AND BOEING DRAWING NR 65C34406. (M) - [SDR AALA981636](https://openairdocs.org/sdr/AALA981636.md): Angle · corroded · Sep 3, 1998 · N889AA · Boeing 727223 · Wing Miscellaneous Structure > TUL - THREE INCH CORROSION SPOT LOWER CHORD BOTTOM SIDE SURFACE AT NR 8 FLAP TRACK ATTACH AREA REAR SPAR. REMOVED CORROSION, ALODINED AND PRIMED. INSTALLED 2024 T-3.071 THICK DOUBLER USING EXISTING PATTERN, THREE ROWS HIGH LOCKS.375 AROUND BLEND AREA, REF - [SDR AALA981635](https://openairdocs.org/sdr/AALA981635.md): Frame · cracked · Sep 3, 1998 · N889AA · Boeing 727223 · Fuselage Main, Frame > TUL - FOUND CRACK ON FRAME AT FS 930 AND STRINGER 14R. INSTALLED DOUBLER AT FS 930 AND STRINGER 14R PER SRM 53-10-2 PAGE 28 E, F, AND G. (M) - [SDR AALA981634](https://openairdocs.org/sdr/AALA981634.md): Skin · corroded · Sep 3, 1998 · N889AA · Boeing 727223 · Fuselage Main, Plate/Skin > TUL - FOUND CORROSION ON SKIN UNDER LEVELING COMPOUND STATION 680-686, STRINGER 26L. REMOVED DAMAGED AREA 1 INCH BY 1 INCH AND INSTALLED DOUBLER PER SRM 53-30-3. (M) - [SDR AALA981633](https://openairdocs.org/sdr/AALA981633.md): Skin · corroded · Sep 3, 1998 · N889AA · Boeing 727223 · Fuselage Main, Plate/Skin > TUL - FOUND CORROSION EMITTING FROM UNDER ICE LIGHT HOUSING, FUSELAGE SKIN CUTOUT. FABRICATED DOUBLER, FILLER DRILLED HOLES, COUNTERSANK HOLES, ALODINED, PRIMED, APPLIED SEALANT AND INSTALLED DOUBLER FILLER AND ICE LIGHT PER SRM 53-30-3 FIG 22 PAGE 137. (M) - [SDR AALA981632](https://openairdocs.org/sdr/AALA981632.md): Skin · corroded · Sep 3, 1998 · N889AA · Boeing 727223 · Fuselage Main, Plate/Skin > TUL - FOUND CORROSION ON FUSELAGE BELLY SKIN UPPER SURFACE OUTBOARD OF STRINGER 28 LT STATION 1010-1015, EXTENDING BELOW STRINGER 28 LT. REMOVED DAMAGED SKIN, INSTALLED FUSELAGE SKIN EXTERNAL REPAIR PER SRM 53-30-3 PAGE 14 FIG 3A, 8 INCHES BY 10 INCHES 7075 T - [SDR AALA981631](https://openairdocs.org/sdr/AALA981631.md): Skin · cracked · Sep 3, 1998 · N889AA · Boeing 727223 · Fuselage Main, Plate/Skin > TUL - FOUND CRACK COMING FROM FASTENER 12 INCHES FORWARD OF STATION 1110 AT NR 2 ENGINE INTAKE DOG HOUSE STRINGER NR 1. CUT OUT DAMAGE SKIN PER SRM 53-30-3 PAGE 12 AND INSTALLED DOUBLER PER BOEING S/B 727-53AD204. (M) - [SDR AALA981630](https://openairdocs.org/sdr/AALA981630.md): Frame · cracked · Sep 3, 1998 · N889AA · Boeing 727223 · Fuselage Main, Frame > TUL - FOUND FUSELAGE FRAME DENTED ABOVE STRINGER 23L, FS 500. INSTALLED BELL FRAME DOUBELR REPAIR PER SRM 51-40-3 PAGE 1 USING 7075T6,.071 THICK 11 INCHES LONG,.375 INCH FASTENER AND 24MS204700 RIVETS, 2 ROWS ON BOTTOM AND ONE ON TOP, 3 RIVETS EACH END. (M - [SDR AALA981629](https://openairdocs.org/sdr/AALA981629.md): Frame · cracked · Sep 3, 1998 · N889AA · Boeing 727223 · Fuselage Main, Frame > TUL - FOUND CRACK STATION 804.95 STRINGER 14R. REMOVED AND REPLACED CRACKED BELL FRAME REINFORCEMENT ANGLE STATION 804.95, STRINGER 14R PER SRM 51-10-1 PAGE 4. (M) - [SDR AALA981628](https://openairdocs.org/sdr/AALA981628.md): Frame · misdrilled · Sep 3, 1998 · N889AA · Boeing 727223 · Fuselage Main, Frame > TUL - FOUND BELL FRAME HEAVY DAMAGE, OVERSIZE FIG 8 HOLE, RIVET TO SMALL, TAILS BENT HOLE GROUND THROUGH BELL FRAME. CUT OUT DAMAGED SECTION ANGLE, INSTALLED ANGLE REPAIR SRM 51-40-3. INSTALLED DOUBLER SRM 51-40-2 AND REPLACED BAD FASTENERS. (M) - [SDR AALA981627](https://openairdocs.org/sdr/AALA981627.md): Frame · dented · Sep 3, 1998 · N889AA · Boeing 727223 · Fuselage Main, Frame > TUL - FOUND BELL FRAME DENTED STATION 1010, BETWEEN STRINGER 26 LT AND 25 LT. INSTALLED BELL FRAME DOUBLER AT STATION 1010, BETWEEN STRINGER 26 LT AND 26 RT PER SRM 51-40-3. (M) - [SDR AALA981626](https://openairdocs.org/sdr/AALA981626.md): Frame · dented · Sep 3, 1998 · N889AA · Boeing 727223 · Fuselage Main, Frame > TUL - FOUND BELL FRAME DENTED. FABRICATED DOUBLER, DRILLED HOLES, TREATED AND PRIMED PER SRM 51-10-2. (M) - [SDR AALA981625](https://openairdocs.org/sdr/AALA981625.md): Web · cracked · Sep 3, 1998 · N889AA · Boeing 727223 · Fuselage Miscellaneous Structure > TUL - FOUND 1.5 INCH CRACK IN WEB BETWEEN 2ND AND 3RD BAY CENTER TANK LBL 13.19 3 INCHES DOWN FROM TOP OF TANK. INSTALLED DOUBLER PER SRM 51-40-2. (M) - [SDR AALA981624](https://openairdocs.org/sdr/AALA981624.md): Shear Tie · corroded · Sep 3, 1998 · N889AA · Boeing 727223 · Fuselage Miscellaneous Structure > TUL - FOUND CORROSION ON SHEAR TIE STATION 950B BETWEEN STRINGER 28RT AND 29 RT. REMOVED DAMAGED SHEAR TIE AND REPAIRED PER SRM 53-10-4. (M) - [SDR AALA981623](https://openairdocs.org/sdr/AALA981623.md): Frame · dented · Sep 3, 1998 · N889AA · Boeing 727223 · Fuselage Main, Frame > TUL - FRAME STATION 700 DENTED ABOVE STRINGER 24R. REMOVED DAMAGE, REPAIRED DOUBLER SRM 51-40-3, FIG 1 SHEET 3 7075-T6,.063 INCH, 10 INCH DOUBLER,.375 AND.25 FASTENERS 20 EACH MS204700 RIVETS 2 ROWS ON SIDE, 1 ROW ON TOP. (M) - [SDR AALA981622](https://openairdocs.org/sdr/AALA981622.md): Frame · dented · Sep 3, 1998 · N889AA · Boeing 727223 · Fuselage Main, Frame > TUL - FUSELAGE BELL FRAME DENTED ABOVE STRINGER 24L AT FS 600. INSTALLED BELL FRAME DOUBLER PER SRM 51-40-3 PAGE 1 USING 7075-T6,.071 INCH THICK, 7 INCHES LONG,.375 INCH AND.25 INCH FASTENERS AND 20 MS 20470D RIVETS, TWO ROWS ON BOTTOM AND ONE RAN ON TOP, - [SDR AALA981621](https://openairdocs.org/sdr/AALA981621.md): Frame · dented · Sep 3, 1998 · N889AA · Boeing 727223 · Fuselage Main, Frame > TUL - BELL FRAME DENTED ABOVE STRINGER 24R AT FS 700. INSTALLED DOUBLER REPAIR PER SRM 51-40-3 FIG 1 SHEET 3 USING 7075 T6,.063 INCH, 10 INCH DOUBLER,.375 FASTENERS AND.25 INCH FASTENER, 20 MS2047AA RIVETS, TWO ROWS ON TOP SIDE AND ONE ROW ON TOP. - [SDR AALA981620](https://openairdocs.org/sdr/AALA981620.md): Frame · dented · Sep 3, 1998 · N889AA · Boeing 727223 · Fuselage Main, Frame > TUL - FUSELAGE BELL FRAME DENTED ABOVE STRINGER 23-24R AT FS 680. INSTALLED REPAIR DOUBLER PER SRM 51-4-3 FIG 1 PAGE 3 USING 7075-T6,.063 INCH THICK, 8 INCH DOUBLER, 21 MS20470D06 RIVETS TWO ROWS PAST DAMAGE AND ONE ROW ON TOP WITH 3 RIVETS AT EACH END. (M) Next page: https://openairdocs.org/deregistered/N889AA-2003-01-08/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 = 'N889AA' AND deregistration_id = 'N889AA-2003-01-08' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N889AA-2003-01-08/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.