# Service difficulty reports: N209US, cancelled Jan 16, 2018

A list on [N209US, cancelled Jan 16, 2018](https://openairdocs.org/deregistered/N209US-2018-01-16.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 · 81 reports

- [SDR P2EA00197](https://openairdocs.org/sdr/P2EA00197.md): Warning Light · illuminated · Jun 4, 2000 · N209US · Boeing 737222 · Door Warning System
  > FLT 780 - MYR - FORWARD CARGO DOOR LIGHT ILLUMINATED JUST AFTER TAKEOFF, RETURNED TO FIELD. LANDING UNEVENTFUL. INSPECTED FORWARD CARGO DOOR CONTACT. CLOSED DOOR, FOUND OPERATIONALLY SATISFACTORY. (M)
- [SDR P2EA00163](https://openairdocs.org/sdr/P2EA00163.md): Skin · dented · May 10, 2000 · N209US · Boeing 737222 · Fuselage Main, Plate/Skin
  > SJO - DURING C-CHECK, FOUND FUSELAGE SKIN AT BS 243 - BS 252.5, BETWEEN WL 170 AND WL 161 RIGHT SIDE, WITH DENT. L= 2.00 FEET, W = 1.50 INCHES, D = 0.063 INCH. REPAIRED FUSELAGE SKIN AT BS 243 - BS 252.5, BETWEEN WL 170 AND WL 161 RIGHT SIDE, IAW SRM 53-30-3
- [SDR P2EA00164](https://openairdocs.org/sdr/P2EA00164.md): Skin · dented · May 10, 2000 · N209US · Boeing 737222 · Fuselage Main, Plate/Skin
  > SJO - DURING C-CHECK, FOUND FUSELAGE SKIN AT BS 438 - BS 447.5, STR 20 - STR 21 LEFT SIDE, WITH DENT. L = 2.00 FEET, W = 1.00 INCH, D - 0.050 INCH. REPAIRED FUSELAGE SKIN AT BS 438 - BS 447.5, STR 20 - STR 21, LEFT SIDE, IAW SRM 53-30-3, FIG 1. SEE COOPESA W
- [SDR P2EA00188](https://openairdocs.org/sdr/P2EA00188.md): Frame · cracked · May 8, 2000 · N209US · Boeing 737222 · Service Doors
  > SJO - DURING C-CHECK, FOUND THE R-2 DOOR LOWER SECTION, LOWER FRAME WITH CRACK 1.5 INCHES LONG,.002 INCHES WIDE. REPLACED THE R-2 DOOR LOWER SECTION, LOWER FRAME IAW BOEING SRM 51-10-1 PAGE 5 AND 51-30-2 PAGE 1. (M)
- [SDR P2EA00193](https://openairdocs.org/sdr/P2EA00193.md): Skin · worn · May 8, 2000 · N209US · Boeing 737222 · Nacelle/Pylon, Plate/Skin
  > SJO - DURING C-CHECK, FOUND THE NR 1 ENGINE NOSE COWL UPPER SECTION SKIN WITH WEAR LENGTH 10 INCH, WIDTH.25 INCH, DEPTH.025 INCH. REPAIRED THE NR 1 ENGINE NOSE COWL UPPER SECTION SKIN IAW COOPESA EO NR COO-3-54-317-00 DATED MAY 12, 2000. (M)
- [SDR P2EA00184](https://openairdocs.org/sdr/P2EA00184.md): Skin · cracked · May 6, 2000 · N209US · Boeing 737222 · Passenger/Crew Doors
  > SJO - DURING C-CHECK, FOUND R-1 DOOR LOWER HINGE SECTION, BS 306-313 BEAM 5-7 SKIN WITH CRACK LENGTH.50 INCH, WIDTH.002 INCH. REPAIRED R-1 DOOR LOWER HINGE SECTION, BS 306-313 BEAM 5-7, SKIN IAW BOEING SERVICE BULLETIN 737-52-1096. (M)
- [SDR P2EA00186](https://openairdocs.org/sdr/P2EA00186.md): Skin · delaminated · May 4, 2000 · N209US · Boeing 737222 · Air Conditioning Doors
  > SJO - DURING C-CHECK, FOUND THE LEFT AIR CONDITION BAY DOOR WITH DELAMINATED, 25 INCHES IN LENGTH, 14 INCHES WIDE. REPAIRED THE LEFT AIR CONDITION BAY DOOR IAW COOPESA EO NR COO-CMP-3-53-305-00 DATED MAY 10, 2000. (M)
- [SDR P2EA00187](https://openairdocs.org/sdr/P2EA00187.md): Panel · delaminated · May 4, 2000 · N209US · Boeing 737222 · Nacelle/Pylon, Plate/Skin
  > SJO - DURING C-CHECK, FOUND THE NR 1 ENGINE PYLON UPPER PANEL WITH DELAMINATED, 14 INCHES IN LENGTH, AND 8 INCHES WIDE. REPAIRED THE NR 1 ENGINE PYON UPPER PANEL IAW COOPESA EO NR COO-CMP-3-57-308-00. (M)
- [SDR P2EA00194](https://openairdocs.org/sdr/P2EA00194.md): Panel · delaminated · May 4, 2000 · N209US · Boeing 737222 · Horizontal Stabilizer, Plate/Skin
  > SJO - DURING C-CHECK, FOUND THE LOWER SKIN OF THE RIGHT HORIZONTAL STAB TRAILING EDGE UPPER PANEL, P/N 65-52493-2 WITH DELAM LENGTH 63 INCHES, WIDTH 6 INCHES. REPAIRED THE LOWER SKIN OF THE RIGHT HORIZONTAL STAB TRAILING EDGE UPPER PANEL P/N 65-52493-2 IAW CO
- [SDR P2EA00183](https://openairdocs.org/sdr/P2EA00183.md): Web · worn · May 2, 2000 · N209US · Boeing 737222 · Fuselage Miscellaneous Structure
  > SJO - DURING C-CHECK, FOUND LOWER FUSELAGE BS 510R, RAM AIR INLET DUCT WEB WITH WEAR 1 INCH IN LENGTH,.50 INCH WIDE,.040 INCH DEEP. REPAIRED LOWER FUSELAGE BS 510R RAM AIR INLET DUCT WEB IAW SRM 51-40-2 FIG 1. (M)
- [SDR P2EA00182](https://openairdocs.org/sdr/P2EA00182.md): Splice · cracked · May 1, 2000 · N209US · Boeing 737222 · Fuselage Miscellaneous Structure
  > SJO - DURING C-CHECK, FOUND STRINGER 27L SPLICE AT BS 358 LBL 16 WITH CRACK.5 INCHES LONG. REPLACED SPLICE FROM BS 354-366 LBL 16 STRINGER 27L IAW SRM 51-10-1 PAR 5. (M)
- [SDR P2EA00180](https://openairdocs.org/sdr/P2EA00180.md): Structure · cracked · Apr 28, 2000 · N209US · Boeing 737222 · Landing Gear Doors
  > SJO - DURIG C-CHECK, FOUND THE LEFT MAIN LANDING GEAR CENTER DOOR TRAILING EDGE WITH CRACK 2 INCHES LONG BY.002 INCHES WIDE. REPAIRED THE LEFT MAIN LANDING GEAR CENTER DOOR TRAILING EDGE IAW SRM 51-40-3 FIG 1. (M)
- [SDR P2EA00181](https://openairdocs.org/sdr/P2EA00181.md): Gate · cracked · Apr 28, 2000 · N209US · Boeing 737222 · Passenger/Crew Doors
  > SJO - DURING C-CHECK, FOUND THE R-2 DOOR UPPER GATE SKIN WITH CRACK 1 INCH IN LENGTH,.001 INCH WIDE. REPLACED THE R-2 DOOR UPPER GATE IAW BOEING MM 52-41-11. (M)
- [SDR P2EA00185](https://openairdocs.org/sdr/P2EA00185.md): Web · cracked · Apr 28, 2000 · N209US · Boeing 737222 · Cargo/Baggage Doors
  > SJO - DURING C-CHECK, FOUND THE FORWARD CARGO DOOR LOWER AFT CORNER WEB WITH CRACK 5.5 INCHES LONG,.002 INCHES WIDE. REPLACED THE LOWER AFT CORNER OF THE FORWARD CARGO DOOR IAW BOEING S/B 737-52-1100 SECTION III FIG 4 REV 2 AND REPAIRED THE CROSSBEAM ON THE
- [SDR P2EA00189](https://openairdocs.org/sdr/P2EA00189.md): Frame · cracked · Apr 28, 2000 · N209US · Boeing 737222 · Service Doors
  > SJO - DURING C-CHECK, FOUND THE R-2 DOOR LOWER SECTION, FORWARD FRAME WITH CRACK 13 INCHES IN LENGTH, WIDTH.002 INCH. REPLACED THE R-2 DOOR LOWER SECTION, FORWARD FRAME IAW BOEING SRM 51-10-1 PAGE 5 AND 51-30-2 PAGE 1. (M)
- [SDR P2EA00191](https://openairdocs.org/sdr/P2EA00191.md): Angle · cracked · Apr 27, 2000 · N209US · Boeing 737222 · Aerodynamic Fairings
  > SJO - DURING C-CHECK, FOUND THE LEFT WING TO BODY FAIRING SUPPORT AT BS 540 STRINGER 22L WITH CRACK 2 INCHES LONG,.001 INCH WIDE. REPLACED THE LEFT WING TO BODY FAIRING SUPPORT AT BS 540 STRINGER 22 IAW BOEING SB 737-53-1098 SECTION III FIG 3 REV 3 DATED JAN
- [SDR P2EA00190](https://openairdocs.org/sdr/P2EA00190.md): Angle · cracked · Apr 27, 2000 · N209US · Boeing 737222 · Aerodynamic Fairings
  > SJO - DURING C-CHECK, FOUND THE RIGHT WING TO BODY FAIRING SUPPORT AT BS 540 STRINGER 22R WITH CRACK 2 INCHES IN LENGTH,.001 INCHES WIDE. REPLACED THE RIGHT WING TO BODY FAIRING SUPPORT AT BS 540 STRINGER 22R IAW BOEING SB 737-53-1098 SECTION III FIG 3 REV 3
- [SDR P2EA00115](https://openairdocs.org/sdr/P2EA00115.md): Line · leaking · Apr 24, 2000 · N209US · Boeing 737222 · Hydraulic System, Main
  > CANCUN - FLT 8009 - LOST A-SYSTEM HYDRAULIC QUANTITY DURING FLIGHT FROM BRO/MRO. DIVERTED TO MMUN (CANCUN) LANDING UNEVENTFUL. REPAIRED.25 INCH HYDRAIULIC LINE PER MM CHAPTER 20, SERVICED HYDRAULIC SYSTEM, LEALK CHECKED OK. (X)
- [SDR P2EA00192](https://openairdocs.org/sdr/P2EA00192.md): Firewall · cracked · Apr 3, 2000 · N209US · Boeing 737222 · Nacelle/Pylon, Bulkhead/Firewall
  > SJO - DURING C-CHECK, FOUND THE NR 2 ENGINE FIREWALL RIGHT SECTION NAC STATION 120 WEB WITH CRACK 3 INCHES LENGTH, WIDTH.006 INCHES. REPLACED THE NR 2 ENGINE FIREWALL RIGHT SECTION NAC STATION 120 WEB P/N 65-53558-8 IAW BOEING SRM 51-10-1 PAGE 5. (M)
- [SDR P2EA00017](https://openairdocs.org/sdr/P2EA00017.md): Control Cable · out of adj · Feb 4, 2000 · N209US · Boeing 737222 · Landing Gear Selector
  > MCI - FLT 299 - AIR RETURN, LANDING UNEVENTFUL. GEAR LEVER WOULD NTO MOVE UP AFTER TAKEOFF. TAKEOFF WARNING DID NOT REMAIN SILENT WITH FLAPS UP. RETURNED TO MCI. ADJUSTED ROD END ON RIGHT MAIN GEAR TELE-FLEX CABLE. PERFORMED GEAR SWING. SYSTEM OPS CHECKS
- [SDR P2EA00005](https://openairdocs.org/sdr/P2EA00005.md): Hinge · worn · Jan 12, 2000 · N209US · Boeing 737222 · Elevator Structure
  > PIT - FLT 578 - F/A REPORTED VIBRATION IN THE BACK OF A/C. IT SEEMS MORE NOTICEABLE ON THE LEFT OF THE A/C. VIBRATION IS ALSO NOTICEABLE IN THE COCKPIT AND IN THE THROTTLES. PERFORMED EVALUATION FLIGHT. DURING EVALUATION FLIGHT, NOTED LOW FREQUENCY VIBRATI
- [SDR 2000ZZZM217](https://openairdocs.org/sdr/2000ZZZM217.md): Bearing · worn · Jan 12, 2000 · N209US · Boeing 737222 · Elevator Structure
  > PIT - FLT 578 - F/A REPORTED VIBRATION IN THE BACK OF A/C. IT SEEMS MORE NOTICEABLE ON THE LEFT OF THE A/C. VIBRATION IS ALSO NOTICEABLE IN THE COCKPIT AND IN THE THROTTLES. PERFORMED EVALUATION FLIGHT. DURING EVALUATION FLIGHT, NOTED LOW FREQUENCY VIBRATI
- [SDR P2EA00001](https://openairdocs.org/sdr/P2EA00001.md): Fire Loop · malfunctioned · Jan 2, 2000 · N209US · Boeing 737222 · Fire Detection
  > BUF - FLT 938 - NR 1 ENGINE OVERHEAT LIGHT ILLUMINATED IN FLIGHT, AFTER THRUST LEVER IS RETARDED TO FLIGHT IDLE THE OVERHEAT LIGHT EXTINGUISHED. AIRCRAFT RETURNED TO GROUND UNEVENTFUL. OVERHEAT SYSTEM CHECKED PER MM 26-10-01, NO DEFECTS NOTED. CHECKED CONDI
- [SDR P2EA99077](https://openairdocs.org/sdr/P2EA99077.md): Gcu · failed · Feb 28, 1999 · N209US · Boeing 737222 · AC Regulator
  > MDW - FLT 703 - ABORTED TAKEOFF AT 103 KNOTS DUE TO FAILURE OF THE NR 1 GENERATOR BUS TRANSFER SYSTEM. THE NR 4 MAIN TIRE BLEW OUT DURING ABORTED TAKEOFF. REMOVED AND REPLACED NR 1 GENERATOR CONTROL UNIT IAW MM 24-21-81. OPS CHECK NORMAL. REMOVED AND REPLA
- [SDR P2EA99073](https://openairdocs.org/sdr/P2EA99073.md): Skin · damaged · Jan 25, 1999 · N209US · Boeing 737222 · Fuselage Main, Plate/Skin
  > SJO - PROVISIONAL REPAIR AT BS 1006, STRINGER 16 RT. REPAIRED FUSELAGE SKIN BETWEEN BS 995 AND BS 1008 FROM STRINGER 14 RT AND STRINGER 16 RT PER SRM SRM 53-30-3 FIG 6. (M)
- [SDR P2EA99072](https://openairdocs.org/sdr/P2EA99072.md): Skin · delaminated · Jan 18, 1999 · N209US · Boeing 737222 · Trailing Edge Flaps
  > SJO - RIGHT WING OUTBOARD AFT FLAP DELAMINATED. DEFECT SIZE LENGTH 1 INCH. REPAIRED FLAP PER SRM 51-40-6, PAR 5 FIG 4. (M)
- [SDR P2EA99069](https://openairdocs.org/sdr/P2EA99069.md): Skin · worn · Jan 18, 1999 · N209US · Boeing 737222 · Engine Cowling System
  > SJO - NR 2 ENGINE NOSE COWL UPPER SKIN SECTION WITH WEAR, DEFECT SIZE LENGTH 10 INCH WIDTH.5 INCH. REPAIRED NR 2 ENGINE COWLING PER SRM 54-30-3, FIG 2. (M)
- [SDR P2EA99034](https://openairdocs.org/sdr/P2EA99034.md): Doubler · disbonded · Jan 14, 1999 · N209US · Boeing 737222 · Fuselage Miscellaneous Structure
  > SJO - INTERNAL DOUBLER DISBONDED FROM BS 616 TO BS 639, STRINGER 8 LT TO STRINGER 9 LT. DEFECT SIZE, LENGTH 23 INCH WIDTH 20 INCH. REPAIRED INTERNAL DOUBLER BETWEEN BS 616 TO BS 639, BETWEEN STRINGER 8 LEFT AND STRINGER 9 LEFT PER SRM 53-30-3, FIG 17. (M)
- [SDR P2EA99033](https://openairdocs.org/sdr/P2EA99033.md): Doubler · disbonded · Jan 14, 1999 · N209US · Boeing 737222 · Fuselage Miscellaneous Structure
  > SJO - INTERNAL DOUBLER DISBONDED FROM BS 616 TO BS 639, BETWEEN STRINGER 8 RT AND STRINGER 9 RT, DEFECT SIZE, LENGTH 23 INCHES, WIDTH 20 INCHES. REPAIRED INTERNAL DOUBLER BETWEEN BS 616 AND BS 639, BETWEEN STRINGER 8 RT AND STRINGER 9 RT PER SRM 53-30-3, FIG
- [SDR P2EA99022](https://openairdocs.org/sdr/P2EA99022.md): Doubler · disbonded · Jan 14, 1999 · N209US · Boeing 737222 · Fuselage Main, Plate/Skin
  > SJO - FUSELAGE SKIN INTERNAL DOUBLER DISBONDED FROM BS 951 TO BS 986.5, BETWEEN STRINGER 6 RT AND STRINGER 8 RT. DEFECT SIZE, LENGTH 34 INCHES, WIDTH 12 INCHES. REPAIRED INTERNAL DOUBLER BETWEEN BS 951 AND BS 986.5, BETWEEN STRINGER 6 RT AND STRINGER 8 RT PE
- [SDR P2EA99020](https://openairdocs.org/sdr/P2EA99020.md): Doubler · disbonded · Jan 14, 1999 · N209US · Boeing 737222 · Fuselage Miscellaneous Structure
  > SJO - INTERNAL DOUBLER DISBONDED FROM BS 951-986.5, BETWEEN STRINGER 6 LEFT AND STRINGER 8 LEFT. DEFECT SIZE, LENGTH 34 INCH, WIDTH 12 INCH. REPAIRED INTERNAL DOUBLER FROM 951 TO BS 986.5, BETWEEN STRINGER LEFT AND STRINGER 8 LEFT PER SRM 53-30-3 FIG 17. (M
- [SDR P2EA99070](https://openairdocs.org/sdr/P2EA99070.md): Fitting · cracked · Jan 10, 1999 · N209US · Boeing 737222 · Emergency Exits
  > SJO - LEFT EMERGENCY EXIT DOOR FORWARD CENTRAL STOP CRACKED, LENGTH.187 INCH. REPLACED STOP FITTING PER SRM 51-10-1 PAGE 5 AND SRM 51-30-2. (M)
- [SDR P2EA99053](https://openairdocs.org/sdr/P2EA99053.md): Frame · cracked · Jan 10, 1999 · N209US · Boeing 737222 · Fuselage Main, Frame
  > SJO - Q-CHECK ITEM. FRAME WEB CRACKED AT BS 351.2 BETWEEN STR 19L AND STR 20L. DEFECT SIZE: LENGTH 0.375 INCH. REPLACED WEB AT BS 351.2 BETWEEN STR 18L AND STR 21L PER SRM 51-10-1 PAGE 5 AND SRM 51-30-2. SEE COOPESA W.O. M1-0003-1-133, VAM 100 NR 662. (X
- [SDR P2EA99032](https://openairdocs.org/sdr/P2EA99032.md): Housing · damaged · Jan 10, 1999 · N209US · Boeing 737222 · Fuel Boost Pump
  > SJO - LEFT WING FUEL TANK, FORWARD CENTER TANK AFT BOOST PUMP HOUSING WITH TEMPORARY REPAIR. REPAIRED LEFT FUEL TANK BOOST PUMP HOUSING PER SRM 57-20-6, FIG 2. (M)
- [SDR P2EA99050](https://openairdocs.org/sdr/P2EA99050.md): Support · worn · Jan 9, 1999 · N209US · Boeing 737222 · Trailing Edge Flaps
  > SJO - Q-CHECK ITEM. RIGHT WING NR 7 CARRIAGE TRACK FAIRING SUPPORT WORN. DEFECT SIZE: LENGTH 2.0 INCHES. DEPTH 0.110 INCH. REWORKED CARRIAGE PER BOEING FAXES COO-SJO-99-0038RR DATED JAN 18, 1999 AND COO-SJO-99-0074RR DATED JAN 22, 1999. DOCUMENTED ON FAA
- [SDR P2EA99049](https://openairdocs.org/sdr/P2EA99049.md): Support · worn · Jan 9, 1999 · N209US · Boeing 737222 · Trailing Edge Flaps
  > SJO - Q-CHECK ITEM. RIGHT WING NR 8 FLAP CARRIAGE FLAP TRACK FAIRING SUPPORT WORN. DEFECT SIZE: LENGTH 1.400 INCHES DEPTH 0.750 INCH. REWORKED CARRIAGE PER BOEING FAXES COO-SJO-99-0038RR DATED JAN 18, 1999 AND COO-SJO-99-0079RR JAN 22, 1999. DOCUMENTED ON
- [SDR P2EA99045](https://openairdocs.org/sdr/P2EA99045.md): Rib · cracked · Jan 9, 1999 · N209US · Boeing 737222 · Wing, Rib/Bulkhead
  > SJO - Q-CHECK ITEM. RIB CRACKED IN LEFT FUEL TANK BETWEEN STIFFENERS 2 AND 3 AT STA 735.5. DEFECT SIZE: LENGTH 2.0 INCHES. REPAIRED RIB LOWER CHORD AT WBL 135.5 AND STR 2 AND STR 3 PER SB 737-57-1166, SEC III, PART III, FIG 3 DATED APRIL 13, 1989. SEE COO
- [SDR P2EA99044](https://openairdocs.org/sdr/P2EA99044.md): Rib · cracked · Jan 9, 1999 · N209US · Boeing 737222 · Wing, Rib/Bulkhead
  > SJO - Q-CHECK ITEM. RIGHT WING, INBOARD MID-FLAP CENTER TRACK RIB CRACKED AT WBL 121. DEFECT SIZE: LENGTH 4.5 INCHES. REPLACED RIB AT WBL 121 RIGHT WING PER 51-10-1, PAGE 5 AND SRM 51-30-2. SEE COOPESA W.O. M1-003-6-43, VAM 100 NR 627. (X)
- [SDR P2EA99041](https://openairdocs.org/sdr/P2EA99041.md): Skin · dented · Jan 8, 1999 · N209US · Boeing 737222 · Wing, Plate/Skin
  > SJO - Q-CHECK ITEM. RIGHT WING LOWER SURACE DENTED AT WBL 260 BETWEEN STIFFENER 6 AND STIFFENER 8. DEFECT SIZE: LENGTH 4.0 INCHES WIDTH 3.0 INCHES DEPTH 0.140 INCH. DENT FOUND STRUCTURALLY SATISFACTORY PER BOEING FAX COO-SJO-99-0043RR DATED JAN 18, 1998.
- [SDR P2EA99026](https://openairdocs.org/sdr/P2EA99026.md): Angle · cracked · Jan 8, 1999 · N209US · Boeing 737222 · Fuselage Miscellaneous Structure
  > SJO - ANGLE CRACKED AT BS 727, RBL 67, WL 208. DEFECT SIZE, LENGTH.375 INCH. FLOOR SUPPORT ANGLE REPAIRED FROM BS 716 TO BS 733, RBL 67, WL 208 PER SRM 51-40-1, FIG 1 DETAIL II. (M)
- [SDR P2EA99010](https://openairdocs.org/sdr/P2EA99010.md): Skin · cracked · Jan 8, 1999 · N209US · Boeing 737222 · Fuselage Main, Plate/Skin
  > SJO - AFT SERVICE DOOR UPPER HINGE CUTOUT CRACKED. DEFECT SIZE, LENGTH.375 INCH. REPAIRED HINGE CUTOUT AREA BETWEEN BS 945.5 TO BS 956, BETWEEN STRINGER 10 RT AND STRINGER 12 RT PER SRM 53-30-3 FIG 21A. (M)
- [SDR P2EA99046](https://openairdocs.org/sdr/P2EA99046.md): Frame · cracked · Jan 7, 1999 · N209US · Boeing 737222 · Fuselage Main, Frame
  > SJO - Q-CHECK ITEM. RIGHT BS 727 CHORD CRACKED AT STR 18A. DEFECT SIZE: LENGTH - 2.125 INCHES. REPLACED RIGHT BS 727 CHORD FITTING BETWEEN STR 18R TO STR 24R PER SB 737-53-1088, SEC III, FIG 2 AND 3, DRAWING NR 65C35722, DATED 12-14-89. SEE COOPESA W.O. M
- [SDR P2EA99042](https://openairdocs.org/sdr/P2EA99042.md): Frame · cracked · Jan 7, 1999 · N209US · Boeing 737222 · Fuselage Main, Frame
  > SJO - Q-CHECK ITEM. BS 727 FUSELAGE OUTBOARD CHORD OF FRAME CRACKED AT STR 18L. DEFECT SIZE: LENGTH: 2.375 INCHES. REPLACED FUSELAGE BS 727 LT CHORD BETWEEN STR 18L TO STR 24L PER SB 737-53-1088, SECTION III, FIG 2 AND FIG 3, AND DRAWING NR 65C33722 DATE 1
- [SDR P2EA99006](https://openairdocs.org/sdr/P2EA99006.md): Stringer · cracked · Jan 7, 1999 · N209US · Boeing 737222 · Fuselage Main, Longeron/Stringer
  > SJO - STRINGER 9RT CRACKED AT BS 1064, WL 270.5, RBL 45. DEFECT SIZE, LENGTH.25 INCH. REPAIRED STRINGER 9RT BETWEEN BS 1056 AND BS 1067 PER SRM 10-3 FIG 2. (M)
- [SDR P2EA99074](https://openairdocs.org/sdr/P2EA99074.md): Bulkhead Skin · cracked · Jan 6, 1999 · N209US · Boeing 737222 · Fuselage Main, Bulkhead
  > SJO - FORWARD PRESSURE BULKHEAD SKIN CRACKED AT BS 178. REPAIRED FORWARD PRESSURE BULKHEAD WEB AT BS 178 BETWEEN LBL 5.7 TO LBL 15.5 WL 231 TO 238.5, BETWEEN RBL 5.7 TO RBL 16 WL 231 TO WL 238.5, BETWEEN RBL 4.5 TO RBL 18.25, WL 216.3 TO WL 224.5 AND BETWEEN
- [SDR P2EA99059](https://openairdocs.org/sdr/P2EA99059.md): Fitting · cracked · Jan 6, 1999 · N209US · Boeing 737222 · Passenger/Crew Doors
  > SJO - Q-CHECK ITEM. MAIN ENTRY DOOR TORQUE TUBE LOWER SUPPORT FITTING CRACKED. DEFECT SIZE: LENGTH 0.500 INCH. REPLACED MAIN ENTRY DOOR STOP FITTING AT BS 294.5, STR 13L PER 51-10-1, PAGE 5 AND SRM 51-30-2. SEE COOPESA W.O. M1-0003-2-123, VAM 100 NR 218.
- [SDR P2EA99047](https://openairdocs.org/sdr/P2EA99047.md): Rib · cracked · Jan 6, 1999 · N209US · Boeing 737222 · Wing, Rib/Bulkhead
  > SJO - Q-CHECK ITEM. RIB CRACKED IN FRONT SPAR CAVITY FSS 390 (SLAT STATION 144.96). DEFECT SIZE: LENGTH 0.500 INCH. REPLACED LEADING EDGE RIB AT SS 144.96 PER SRM 51-10-1, PAGE 5, AND SRM 51-30-2. SEE COOPESA W.O. M1-0003-5-69, VAM 100 NR 313 FOR TECHNICAL
- [SDR P2EA99031](https://openairdocs.org/sdr/P2EA99031.md): Frame · cracked · Jan 6, 1999 · N209US · Boeing 737222 · Fuselage Main, Frame
  > SJO - FRAME LOWER FLANGE CRACKED AT BS 440, BETWEEN STRINGER 28 LEFT AND STRINGER 28 RT, DEFECT SIZE, LENGTH.50 INCH. REPAIRED FRAME SECTION AT BS 440, BETWEEN STRINGER 28 LEFT AND STRINGER 28 RT PER SRM 53-10-4, FIG 10. (M)
- [SDR P2EA99025](https://openairdocs.org/sdr/P2EA99025.md): Rib · cracked · Jan 6, 1999 · N209US · Boeing 737222 · Leading Edge Devices
  > SJO - LEADING EDGE FSS 594, NR 1 SLAT OUTBOARD MAIN TRACK, RIB CRACKED. DEFECT SIZE, LENGTH.0125 INCH. REPLACED RIB AT FSS 594 PER SRM 51-10-1 PAGE 5 AND SRM 51-30-2. (M)
- [SDR P2EA99024](https://openairdocs.org/sdr/P2EA99024.md): Splice · cracked · Jan 6, 1999 · N209US · Boeing 737222 · Fuselage Miscellaneous Structure
  > SJO - STRINGER 10 LEFT SPLICE CRACKED AT BS 544, DEFECT SIZE, LENGTH.50 INCH. REPAIRED STRINGER 10 LEFT SPLICE BETWEEN BS 538 TO BS 550 PER SRM 51-10-1, PAGE 5 AND SRM 51-30-2. (M)

Next page: https://openairdocs.org/deregistered/N209US-2018-01-16/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 = 'N209US' AND deregistration_id = 'N209US-2018-01-16'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N209US-2018-01-16/reports

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